Title of Invention

CONTROL SYSTEM FOR HYBRID POWERTRAIN

Abstract A method and apparatus for determining a preferred operating range for a plurality of torque-generative devices is provided. Each device is operable to provide motive torque to a transmission, The invention includes defining a first and a second operating range in a first operating space. The first operating range and the second operating range are mathematically transformed to a second operating space. The preferred operating range is defined in the second operating space based upon the transformed first operating range and the transformed second operating range. The first operating range is defined based upon torque output for each of the torque-generative devices, The second operating range is defined based upon output of an electrical energy storage device operable to provide electrical energy to each of the torque-generative devices.
Full Text

FIELD OF THE INVENTION
This invention pertains generally to vehicle powertrain systems, and more specifically to
a control system for a hybrid transmission system for a vehicle.
BACKGROUND OF THE INVENTION
Various hybrid powertrain architectures are known for managing the input and output
torques of various prime-movers in hybrid vehicles, most commonly internal combustion
engines and electric machines. Series hybrid architectures are generally characterized by
an internal combustion engine driving an electric generator which in turn provides
electrical power to an electric drivetrain and to a battery pack. The internal combustion
engine in a series hybrid is not directly mechanically coupled to the drivetrain. The
electric generator may also operate in a motoring mode to provide a starting function to
the internal combustion engine, and the electric drivetrain may recapture vehicle braking
energy by also operating in a generator mode to recharge the battery pack. Parallel hybrid
architectures are generally characterized by an internal combustion engine and an electric
motor which both have a direct mechanical coupling to the drivetrain. The drivetrain
conventionally includes a shifting transmission to provide the preferable gear ratios for
wide range operation.

One hybrid powertrain architecture comprises a. two-mode, compound-split, electro-
mechanical transmission which utilizes an input member for receiving power from a
prime mover power source and an output member for delivering power from the
transmission, typically to a vehicle driveline. First and second motor/generators are
pperatively connected to an energy storage device for interchanging electrical power
between the storage device and the first and second motor/generators. A control unit is
provided for regulating the electrical power interchange between the energy storage
device and the first and second motor/generators. The control unit also regulates,
electrical power interchange . between the first and second motor/generators.
Engineers implementing hybrid powertrain systems attempt to meet fuel economy and
emissions targets by determining engine power from a required road-load power plus an
additional quantity of engine power based on the energy storage system's (e.g. battery's)
state-of-charge. Following determination of engine power, the engine's optima) fuel
economy or optimal emissions map, or a combination thereof, may be used to select the
engine's torque/speed operating point. The battery power used by the system is that which
is required, in combination with the engine power, to meet the road-load power
requirements and to compensate for power losses within the system.

Some known systems do not simultaneously optimize power flow from all the propulsion
system components. Typically, only engine operation is optimized. Additional factors
such as system mechanical and electrical losses and battery usage factors are often not
used in selecting the overall system's preferred operating point. Systems which attempt to
account for system meshanical and electrical losses and. battery usage, factors in
optimizing power flow of all propulsion system components have faced a daunting task
of simultaneously calculating the various power flows, consuming substantial amounts of
on-board computer processing resources, both in terms of processing time and
throughput, and algorithm complexity.
Therefore, there is a need to develop a hybrid powertrain control system which can
optimize power flow from all the propulsion system components, accounting for losses,
in a manner which effectively uses on-board computing resources.
OBJECT OF THE INVENTION
It is therefore an object of this invention to provide a hybrid powertrain control system
which optimizes power flow from all the propulsion system components, accounting for
losses, in a manner which effectively uses on-board computing resources. SUMMARY OF THE INVENTION
Thus, in accordance with the invention, an article of manufacture is provided, comprising
a storage medium having a computer program encoded therein for effecting a method to
determine a preferred operating range for a plurality of torquergenerative devices. Each
of the torque-generative devices is operable to provide motive torque to a torque
transmission device. The

program comprises code for defining a first and a second operating range in a first
operating space. The first operating range and the second operating range are
mathematically transformed to a second operating space. The preferred operating range is
defined in the second operating space based upon the transformed first operating range
and the transformed second operating range.
An aspect of the invention includes defining the first operating range based upon torque
output for each of the torque-generative devices.
Another aspect of the invention includes defining the second operating range based upon
output of an electrical energy storage device operable to provide electrical energy to each
of the torque-generative devices;
Another aspect of the invention comprises defining the operating range based upon
output of the electrical energy storage device and electrical energy system constraints,
which further comprises limiting electrical energy transmission to the electrical energy
storage system to limit charging of the electrical energy storage device, and to limit
discharging of the electrical energy storage device.
Another aspect of the invention comprises transforming the first operating range and the
second operating range to the second operating space, which includes linearly
transforming the first operating range and the second operating range from a radial
dimension to an XY dimension.
Another aspect of the invention comprises retransforming the defined preferred operating
range to the first operating space.
Another aspect of the invention comprises determine the preferred operating range for the
torque-generative devices during a cycle time less than about twelve milliseconds.

Another aspect of the invention includes the torque-generative devices comprising a pair
of eieptrical motor/generators, and the torque transmission device comprises a two-mode
compound split hybrid electron-mechanical transmission which is operable to transmit
motive torque to a drivejine of a vehicle,
These and other aspects of the invention will become apparent to those skilled in the art
upon reading and understanding the following detailed description of the embodiments.
BRIEF DESCRIPTION OF THE ACCOMPANYING DRAWINGS
. The invention may take physical form in certain parts and arrangement of parts, the
preferred embodiment of which wjll be described in detail and illustrated in the
accompanying drawings which form a part hereof, and wherein:
FIG. 1 is a schematic diagram of an exemplary powertrain, in accordance with the present
invention;
FIG. 2 is a schematic diagram of an exemplary control architecture and powertrain, in
accordance with the present invention;
FIG. 3 is an analysis diagram, in accordance with the present invention; and,
FIGS. 4 and 5 are representative data graphs, in accordance with the present invention.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
Referring now to the drawings, wherein the showings are for the purpose of illustrating
the invention only and not for the purpose of limiting,the same, FIGS. 1 and 2 show a
system comprising an engine 14, transmission 10, control system, and driveline which
has been constructed in accordance with an embodiment of the present invention.
Mechanical aspects of exemplary transmission 10 are disclosed in detail in commonly
assigned U.S. Patent Application Publication No. U.S. 2005/0137042 A I, published Jun.
23, 2005, entitled Two^Mode, Compound-Split, Hybrid Electro-Mechanical
Transmission having Four Fixed Ratios, which is incorporated herein by reference. The
exemplary two^mode, compound-split, electrormechanical hybrid transmission
embodying the concepts of the present invention is depicted in FIG. I, and is designated
generally by the numeral 10. The hybrid transmission 10 has an input member 12 that
may be in the nature of a shaft which may be directly driven by an engine 1.4. A transient
torque damper 20 is incorporated between the output shaft 18 of the engine 14 and the
input member 12 of the hybrid transmission 10. The transient torque damper 20
preferably comprises a torque transfer device 77 having characteristics of a damping
mechanism and a spring, shown respectively as 78 and 79. The transient torque damper
20 permits selective engagement of the engine 14 with the hybrid transmission 1Q, but it
must be understood that the torque transfer device 77 is not utilized to change, or control,
the mode in which the hybrid transmission 10 operates, The torque transfer device 77
preferably comprises a hydraulically operated friction clutch, referred to as clutch C5.

The engine 14 may be any of numerous forms of internal combustion engines, such as a
spark-ignition engine or a compression-ignition engine, readily adaptable to provide a
power output to the transmission 10 at a range of operating speeds, from idle, at or near
600 revolutions per minute (RPM), to over 6,000 RPM. Irrespective of the means by
which the engine 14 is connected to the input member 12 of the transmission 10, the
input member 12 is connected to a planetary gear set 24 in the transmission 10.
Referring specifically now to FIG. 1, the hybrid transmission 10 utilizes three planetary*
gear sets 24, 26 and 28, The first planetary gear set 24 has an outer gear member 30 that
may generally be designated as a ring gear, which circumsqribes an inner gear member
32, generally designated as a sun gear. A plurality of planetary gear members 34 are
rotatably mounted on a carrier 36 such that each planetary gear member 34 meshingly
engages both the outer gear member 30 and the inner gear member 32.
The second planetary gear set 26 also has an outer gear member 38, generally designated
as a ring gear, which circumscribes an inner gear member 40, generally designated as a
sun gear. A plurality of planetary gear members 42 are rotatably mounted on a carrier 44
such that each planetary gear 42 meshingly engages both the outer gear member 38 and
the inner gear member 40.
The third planetary gear set 28 also has an outer gear member 46, generally designated as
a ring gear, which circumscribes an inner gear member 48, generally designated as a sun
gear. A plurality of planetary gear members 50 are rotatably. mounted on a carrier 52 such
that each planetary gear 50

rneshingiy engages bath the outer gear member 46 and the inner- gear member 48.
Ratios of teeth on ring gears/sun gears are typically based upon design considerations
known to skilled practitioners and outside the scope of the present invention. By way of
example, in one embodiment, the ring gear/sun gear tooth ratio of the planetary gear set
24 is 65/33; the ring gear/sun gear tooth ratio of the planetary gear set 26 is 65/33; and
the ring gear/sun gear tooth ratio of the planetary gear set 28 is 94/34-
The three planetary gear sets 24, 26 and 28 each comprise simple planetary gear sets.
Furthermore, the first and second planetary gear sets 24 and 26 are compounded in that
the inner gear member 32 of the first planetary gear set 24 is conjoined, as through a hub
plate gear 54, to the outer gear member 38 of the second planetary gear set 26. The
conjoined inner gear member 32 of the first planetary gear set 24 and the outer gear
member 38 of the second planetary gear set 26 are continuously connected to a first
motor/generator 56, also referred to as 'Motor AThe planetary gear sets 24 and 26 are further compounded in that the carrier 36 of the
first planetary gear set 24 is conjoined, as through a shaft 60, to the carrier 44 of the
second planetary gear set 26. As such, earners 36 and 44 of the first and second planetary
gear sets 24 and 2,6, respectively, are conjoined. The shaft 60 is also selectively
connected to the carrier 52 of the third planetary gear set 28, as through a torque transfer
device 62 which, as will be hereinafter more fully explained, is employed to assist in the .
selection of the operational modes of the hybrid transmission 10. The carrier 52 of the

third planetary gear set 28 is connected, directly to the transmission output member 64.
In the embodiment described herein, wherein the hybrid transmission 10 is used in a land
vehicle, the output member 64 i§ operably connected to a driveline comprising a gear box
90 or other torque transfer device which provides a torque output to one or more
vehicular axles 92 or half-shafts (not shown). The axles 92, in turn, terminate in drive
members 96. The drive members 96 may be either front or rear wheels of the vehicle on
which they are employed, or they may be a drive gear of a track vehicle. The drive
members 96 may have some form of wheel brake 94 associated therewith. The drive
members each have a speed parameter, N.sub.WHL, comprising rotational speed of each
wheel 96 which is typically measurable with a wheel speed sensor.
The inner gear member 40 of the second planetary gear set 26 is connected to the inner
gear member 48 of the third planetary gea.r set 28, as through a sleeve shaft 66 that
circumscribes shaft 60. The outer gear member 46 of the third planetary gear set 28 is
selectively connected to ground, represented by the transmission housing 68, through a
torque transfer device 70. Torque transfer device 70, as is also hereinafter explained, is
also employed to assist in the selection of the operational modes of the hybrid
transmission 10. The sleeve shaft 66 is also continuously connected to a second
motor/generator 72, also referred to as 'Motor B
All the planetary gear sets 24, 26 and 28 as well as the two motor/generators 56 and 72
are coaxiajly oriented, as about the axially disposed shaft 60. Motor/generators 56 and 72
are both of an annular configuration which permits them-to circumscribe the three
planetary gear sets 24, 26 and 28 such that the planetary gear sets 24, 26 and 28 are
disposed radially inwardly of the motor/generators 56 and 72. This configuration assures
that the. overall envelope,.i.e., the circumferential dimension, of the transmission 10 is
minimized.
A torque transfer device 73 selectively connects the sun gear 40 with ground, i.e., with
transmission housing 68. A torque transfer device 75 is operative as a lock-up clutch,
locking planetary gear sets 24, 26, motors 56, 72 and the input to rotate as a group, by
selectively connecting the sun gear 40 with the carrier 44. The torque transfer devices 62,
70, 73, 75 are all friction clutches, respectively referred to as follows: clutch CI 70,
clutch C2 62, clutch C3 73, and clutch C4 75. Each clutch is preferably hydraulically
actuated, receiving pressurized hydraulic fluid from a pump. Hydraulic actuation is
accomplished using a known hydraulic fluid circuit, which is not described in detail
herein,
The hybrid transmission 10 receives input motive torque from a plurality of torque-
generative devices, including the engine 14 and the motors/generator? 56 and 72, as a
result of energy conversion from fuel or electrical potential stored in an electrical, energy
storage device (ESD) 74, The ESD 74 typically comprises one or more batteries. Other
electrical energy and electrochemical energy storage devices that have the ability to store
electric power and dispense electric power may be used in place of the batteries

without altering the concepts of the present invention. The ESD 74 is preferably sized
based upon factors including regenerative requirements, application issues related to
typical road grade and temperature, and propulsion requirements such as emissions,
power assist and electric range. The ESP 74 is high voltage TJ>C-coupled to transmission
power inverter module (TPIM) 19 via DC lines or.transfer conductors 27, The TPIM 19
is an element of the control, system described hereinafter with regard to FIG. 2. The
. TPIM 19 communicates with the first motor/generator 56 by transfer conductors 29, and
the TPIM 19.similarly communicates with the second motor/generator 72 by transfer
conductors 31. Electrical current is transferable to or from the ESD 74 in accordance with
whether the ESD 74 is being charged or discharged. TPIM 19 includes the pair of power
inverters and respective motor controllers configured to receive motor control commands
and control inverter states therefrom for providing motor drive or regeneration
functionality.
In motoring control, the respective inverter receives current from the DC lines and
provides AC current to the respective motor over transfer conductors 29 and 31. In
regeneration control, the respective inverter receives AC current from the motor over
transfer conductors 29 and 31 and provides current to the DC lines 27. The net DC
current provided to or from the inverters determines the charge or discharge operating
mode of the electrical energy, storage device 74. Preferably, Motor A 56 and Motor B 72
are three-phase AC machines and the inverters comprise complementary three-phase
power electronics.

Referring again to FIG. 1, a drive gear 80 may be presented from the input member 12.
As depicted, the drive gear 80 fixedly connects the input member 12 to the outer gear
member 30 of the first planetary gear set 24, and the drive gear 80, therefore, receives
power from, the engine 14 and/or the motor/generators 56 and/or 72 through planetary
gear sets 24 and/or 26, The drive gear 80 meshingly engages an idler gear 82 which, in
turn, meshingly engages a transfer gear 84 that is secured to one end of a shaft 86. The
other end of the shaft 86 may be secured to a hydraulic/transmission fluid pump and/or
power take-off ('PTO') unit, designated either individually or collectively at 88, and
comprise an accessory load.
Referring now tp FIG. 2, a schematic block diagram of the control system, comprising a
distributed controller architecture, is shown. The elements described hereinafter comprise
a subset of an overall vehicle control architecture, and are operable to provide
coordinated system control of the powertrain system described herein. The control system
is operable to synthesize pertinent information and inputs, and execute algorithms to
control various actuators to achieve control targets, including such parameters as fuel
economy, emissions, performance, driveability, and protection of hardware, including
batteries of ESD 74 and motors 56, 72- The distributed controller architecture includes
engine control module ('EClVf) 23, transmission control module (TCM') 17, battery
pack control module OBPCiVr) 21, and Transmission Power Inverter Module (TPUVT)
19. A hybrid control module ('HCP') 5 provides overarching control and coordination of
the aforementioned controllers. There is a User Interface ('UF) 13 operably connected to
a plurality of devices through which a vehicle operator typically

controls or directs operation of the powertrain, including the transmission 10. Exemplary
vehicle operator inputs to the UI 13 include an accelerator pedal, a brake pedal,
transmission gear selector, and, vehicle speed cruise control. Each of the aforementioned
controllers communicates with other controllers, sensors, and actuators via a local area
network (XAN') bus 6. The LAN bus 6 allows for structured communication of control
parameters and commands between the various controllers. The specific communication
protocol utilized is application-specific, By way of example, one communications
protocol is the Society of Automotive Engineers standard J1939. The LAN bus and
appropriate protocols provide for robust messaging and multHControlIer interfacing
between the aforementioned controllers, and other controllers providing functionality
such as antilock brakes, traction control, and vehicle stability.
The HCP 5 provides overarching control of the hybrid powertrain system, serving to
coordinate operation of the ECM 23, TCM 17, TP1M 19, and BPCM 21. Based upon
various input signals from the UI 13 and the powertrain, the HCP 5 generates various
commands, including: an engine torque command, T.sub.E.sub.--.sub.CMD; clutch
torque commands, T.sub.CL.sub.—.sub.N for the various clutches CI, C2, C3, C4 of the
hybrid transmission 10; and motor torque commands, T.sub.A.sub.--.sub.CMD and
T.sub.B.sub.--.sub.CMD, for the electrical Motors A and B, respectively.
The ECM 23 is operably connected to the engine 14, and functions to acquire data from a
variety of sensors and control a variety of actuators, respectively, of the engine 14 over a
plurality of discrete lines collectively shown as aggregate line 35. The ECM 23 receives
the engine torque

command, T.sub.E.sub.^sub.CMD, from the HCP 5, and generates a desired axle torque,
T,sgb.AXLE.sub.->-rsu{3.QES, and an indication of actual engine torque, T.sub.E, which is
communicated to the HCP 5. For simplicity, ECM 23 is shown generally having bir
directional interface with engine 14 via aggregate line 35. Various other parameters that
may be sensed by ECM 23 include engine coolant temperature, engine input speed
(N.sub,E) to a shaft leading to the transmission, manifold pressure, ambient air
temperature, and ambient pressure. Various actuators that may be controlled by the, ECM
23 include fuel injectors, ignition modules, and throttle control modules.
The TCM 17 is operably connected to the transmission 10 and functions to acquire data
from a variety of sensors and provide command signals to the transmission. Inputs from
the TCM 17 to the HCP § include estimated clutch torques, T.sub.CL.gub.-.sub.N.sub.-r
, sub, EST, for each of the clutches CI, C2, C3, and, C4 and rotatipnal speed., N.sub.O, of
the output shaft 64r Other actuators and sensors may be used to provide additional
information from.the TCM to the HCP for control purposes.
The BPCM 21 is signally connected one or more sensors operable to monitor electrical
current or voltage parameters of the ESD 74 to provide information about the state of the
batteries to the HCP 5. Such information includes battery state-of-charge, Bat_S0C, and
. other states of the batteries., including voltage, V.sub.BAT, and available power,
P.sub.BAT.sub.-.,§ub.M!N and P,sub.BAT,sub.--.sub.MAX!
The Transmission Power Inverter Module (TPJM) 19 include? a pair of power inverters
and motor controllers configured to receive motor control comrnands and control inverter
states therefrom to provide motor drive or regeneration functionality. The TPJM 19 is
operable to generate torque

commands for Motors A and B, T.subA.sub.--.sub.CMD and T.sub.J3.sub.--.sub.CMD,
based upon input from the HCP 5, which is driven by operator input through Ul 13 and
system operating parameters. The predetermined torque commands for Motors A and B,
T.sub.A.sub.--.sub.CMD and T.sub-B.sub.~-.sub.CMD, are adjusted with motor damping
torques, T,sub,A.sub.--.sub.DAMP and T.sub.B.sub.-.sub.DAMP, to determine motor
torques, T.sub,A and T.siib.B, which are implemented by the control system, including
the TPIM 19, to.control the Motors A and B. Individual motor speed signals, N.sub.A and
Ksub.B for Motor A and Motor B respectively, are derived by the TPIM 19 from the
motor phase information or conventional rotation sensors. The TPIM 19 determines and
communicates motor speeds, N.sub.A and N.sub.B, to the HCP 5. The electrical energy
storage device 74 is high-voltage DC-coupled to the TPIM 19 via DC lines 27. Electrical
current is transferable to or from the TPIM 19 in accordance with whether the ESD 74 is
being charged or discharged,,
Each of the aforementioned controllers is preferably a general-purpose digital computer
generally comprising a microprocessor or central processing unit, read only memory
(ROM), random acpess memory (RAM), electrically programwable read only memory
(EPROM), high speed clock, analog to digital (A/D) and digital to analog (D/A) circuitry,
and input/output circuitry and devices (I/O) and appropriate signal conditioning and
buffer circuitry. Each controller has a set of control algorithms, comprising resident
program instructions and calibrations stored in ROM and executed to provide the
respective functions of each computer. Information transfer between the various
computers is preferably accomplished using the aforementioned LAN 6.

Algorithms for control and state estimation in each of the controllers are typically
executed during preset loop cycles such that each algorithm is executed at least once each
loop cycle. Algorithms stored in the non-volatile memory devices are executed by one of
the central processing units and are operable to monitor inputs from the sensing devices
and execute control and diagnostic routines to control operation of the respective device,
using preset calibrations. Loop cycles are typically executed at regular intervals, for
example each 3, 6.25, 15, 25 and 100 milliseconds during ongoing engine and vehicle
operation. Alternatively, algorithms may be executed in response to occurrence of an
event.
In response to an operator's action, as captured by the UI 13, the supervisory HCP
controller 5 and one or more of the other controllers determine required transmission
output torque, T.sub.O. Selectively operated components of the hybrid transmission 10
are appropriately controlled and manipulated to respond to the operator demand. For
example, in the exemplary embodiment shown in FIGS, 1 and 2, when the operator has
selected a forward drive range and manipulates either the accelerator pedal or the brake
pedal, the HCP 5 determines an output torque for the transmission, which affects how and
when the vehicle accelerates, or decelerates. Final vehicle acceleration is affected by other
factors, including, e.g., road load, road grade, and vehicle mass. The HCP 5 monitors the
parametric states of the torque-generatjve devices, and determines the output of the
transmission required to arrive at the desired torque Output. Under the direction of the
HCP 5, the transmission 10 operates over a range of output speeds from slow to fast in
order to meet the operator demand.

The tworniode, compounds-split, electro-mechanical hybrid transmission, includes output
member 64 which receives output power through two distinct gear trains within the
transmission 10, and operates in several transmission operating modes, described with
reference now to FIG. 1, and Table 1, below.
TABLE^US-00001 TABLE 1 .
Transmission Operating Mode Actuated Clutches
Mode I CI 70
Fixed Ratio 1 CI 70 C4 75
Fixed Ratio 2 CI 70 C2 62
Mode II C2 62
Fixed Ratio 3 C2 62 C4 75
Fixed Ratio 4 C2 62 C3 73
The various transmission operating modes described in the table indicate which of the
specific clutches CI, C2, C3, C4 are engaged or actuated for each of the operating modes.
Additionally, in various transmission operating modes, Motor A 56 or Motor B 72 may
each operate as electrical motors, designated as MA, MB respectively, and whether
Motor A 56 is operating as a generator, designated as GA. A first mode, or gear train, is
selected when the torque transfer device 70 is actuated in order to "ground" the outer gear
member 46 of the third planetary gear set 28. A second.mode, or gear train, is selected
when the torque transfer device 70 is released and the torque transfer device 62 is
simultaneously actuated to connect the shaft 60 to

the carrier 52 of the third planetary gear set 28. Other factors outside the scope of the
invention affect when the electrical machines 56, 72 operate as motors and generators,
and are not discussed herein.
The control system, shown primarily in FIG. 2,. is operable to provide a range of
•3 S
. transmission output speeds, TM.sub.O, of shaft 64 from relatively slow to relatively fast
within each mode of operation. The combination of two modes with a slow-to-fast output
speed range in each mode allows the transmission 10 to propel a vehicle from a stationary
condition to highway speeds, and meet various other requirements as previously
described. Additionally, the control system coordinates operation of the transmission 10
so as to allow synchronized shifts between the modes.
The first and second modes of operation refer to circumstances in which the transmission
functions are controlled by one clutch, i.e. either clutch CI 62 or C2 70, and by the
controlled speed and torque of the motor/generators 56 and 72. Certain ranges of
operation are described below in which fixed ratios are achieved by applying an
additional clutch. This additional clutch may be clutch C3 73 or C4 75, as shown in the
table, above.
When the additional clutch is applied, fixed ratio of inputrto-output speed of the
transmission, i.e. "N.sub.I/N.sub.O, is achieved. The rotations of the motor/generators 56,
72 are dependent on internal rotation of the mechanism as defined by the clutching and
proportional to the input speed, N.sub.l, determined or measured at shaft 12. The
motor/generators function as motors or generators. They are completely independent of
engine to output power flow, thereby enabling both to be motors, both to function as
generators, or any combination thereof. This allows, for instance, during operation in
Fixed Ratio

1 that motive power output from the transmission at shaft 64 is provided.by power from
the engine and power from Motors A and B, through planetary gear set 28 by accepting '
power from the energy storage device 74.
The transmission operating mode can be switched between Fixed Ratio operation and
Mode operation by activating or deactivating one the additional clutches during Mode I
or Mode II operation. Determination of operation in fixed ratio or mode control is by
algorithms executed by the control system, and is outside the scope of this invention.
The modes of.operation may overlap the ratio of operation, and selection depends again
on the driver's input and response of the vehicle to that input. RANGE 1 falls primarily
within mode I operation when clutches CI 70 and C4 75 are engaged. RANGE 2 falls
within mode ! and mode II when clutches C2 62 and CI 70 are engaged. A third fixed
ratio range is available primarily during mode 11 when.clutches C2 62 and C4 75 are
engaged, and a fourth fixed ratio range is available during mode II when clutches C2 62
and C3 73 are engaged. It is. notable that ranges of operation for Mode I and Mode II
typically overlap significantly.
Output of the exemplary powertrain system described hereinabove is constrained due to
mechanical and system limitations. The output speed, N.sub.O, of the transmission
measured at shaft 64 is limited due to limitations of engine output speed, N.sub.E,
measured at shaft 18, and transmission input speed, N.sub.I, measured at shaft 12, and
speed limitations of the electric Motors A and B, designated as +/- N.sub.A, +/- N.sub.B.
Output torque, T.sub.O, of the transmission 64 is similarly limited due to limitations of
the engine input torque, T.sub.E, and input torque, T.sub.I, measured at shaft 12 after the
transient torque damper 20, and .

torque limitations (T.sub.A.sub.-.sub.MAX, T.sub.A-sub.-.sub.MIN, T.sub.B.sub.^-
.sub.MAX, T.sub.B.sub.-.sub.MI'N) of the Motors A and B S6, 72.
The various equations and. operations described herein are preferably executed as
. algorithms in one or more of the controllers described hereinabove with reference to FIG.
2. In the present embodiment of the invention, it is an objective to determine a range of
allowable operating points for Motor A 56 and Motor B 72. The allowable operating
points are preferably described in terms of motor torques, T-sub.A and T.sub.B, of
electrical transmission 10 operative to provide motive torque in the hybrid powertrain
system.
The invention comprises a method, stored and executed as one or more algorithms in one
or more of the controllers of the control system, to determine a preferred operating range
for the torque^generatjve devices, i,e. Motors A and B 56, 72, as executed in the
exemplary system. The operation comprises defining a first operating range in a first
operating space, and defining a second operating range in the first operating space. The
first operating range and the second operating range are transformed to a second
operating space, The preferred operating range is defined in the second operating space
based upon the transformed first operating range and the transformed second operating
range. The first operating range is preferably defined as a torque output of Motors A and
B, and the second operating range is preferably defined as the electrical power output
from the ESD in this embodiment. The first operating range and the second operating
range are transformed to the second operating space, which is preferably in what is
referred to as TX/TY space. The preferred operating range in the second operating space
is based upon the transformed first operating range and the

transformed second operating range. This is shown hereinafter, with reference now to
FIG. 5 and the equations which follow.
The first operating range is defined as a torque output range for the Motor A 56
(T^ub.A.sub.-.sub.MAX, T.sub.A.sub,--.sub.MTN) and, a torque output range for the
Motor B 72 (T.sub.B.sub.-.sub.MAX, T.sub.B.sub.-.sub.MlN). The first operating range
thus comprises the torque operating range bounded by motor torque constraints
T.sub.A.sub.*-,sub.MAX, T.sub.A.sub.-.sub.MrN, T.sub.B.sub.-.sub.MAX,
T.sub.B.sub.-.sub.MIN. With reference to FIG. 3, the first operating space 110 is shown,
wherein values T.sub.A.sub.—.sub.MAX 114, T.sub.A.sub.—.sub-MIN 112, T.sub.B.sub.-'
-,sub.MAX 118, T.sub.B.sub.-.sub.MlW 116 are plotted.
Minimum and maximum motor torques (T.sub.A.sub.^-.sub.MAX, T.sub.A.sub.-^
.sub.MIN, T.sub.B.sub.-.sub.MAX, T.sub.B.sub.-r.sub.MIN) within the present
capabilities of the motors are preferably obtained from data sets stored in table form
within data structures in the control system. Such data sets are provided for reference by
the routine in pre-stored table format having been empirically derived from conventional
dynamometer testing of the combined motor and power electronics (e.g. power inverter)
at various temperature and voltage conditions. An exemplary representation of such
characteristic motor torque vs, speed data is illustrated in FIG. 4 wherein minimum and
maximum data for a given speed are represented by the line of constant speed 132
intersecting exemplary lines of constant temperature/voltage 131, 133. The tabulated data
is referenced by the motor speeds (N.sub.A, "N.sub.B), voltage and temperature.
While the motors are used in both motoring and generating modes—suggesting four-
quadrants (identified as 1, 11, III, IV with reference to FIG. 4) of torque/speed data—two
quadrant data collection is generally sufficient wherein the data collected in adjacent
quadrants is merely reflected in the other quadrants not directly measured. In the present
example, quadrants I and

IV are shown with determined data 13! whereas quadrants III and IV are shown
populated with data 133 reflected across the torque axis.
Exemplary data for motor torques is shown. Motor A torque, T.sub.A, is plotted across
•r-
the horizontal axis and Motor B torque, T.sub.B, is" plotted across the vertical axis.
"'(/■
■ f>
Boundaries are drawn as dotted lines corresponding to minimum and maximum Motor A
torques (T.sub.A.sub.--.su.b.MAX, T.sub.A.sub.--.sub.MIN), the minimum and maximum
being with respect to motor capabilities at certain exemplary present operating conditions
in N.sub.l, N.sub.O, the.precise values of which are not required for the present
exposition of the teachings to be gained from FIG. 5 and the present discussion. Similar
boundaries are drawn as dotted lines corresponding to such minimum and maximum
Motor B torques (T.sub.B.sub.--.sub.MAX, T.sub.B,sub.--.sub.MIN). The enclosed space
represents a feasible solution space at present conditions for Motor A 56 and Motor B 72.
Once again, the precise values used herein are not critical to the understanding to be
gained from the present description and figure, but are provided for appropriate context
and to redupe the teaphing's abstraction,
A second operating range, comprising a torque output range, shown as 120 with reference
to FIG. 3, is determinable based upon constraints of the electrical energy storage system
74. Calculation of battery power, P.sub.BAT is as follows, in Eq. 3:
P.sub!BAT=P.sub.A,ELEC+P.sub.B,ELEC+P.sub.DC.sub.-.subXOAD[3]
wherein: P.sub.A,ELEC comprises electrical power from Motor A; P.sub.B,ELEC
comprises electrical power from Motor B; and, P.sub.DC.sub.-*.sub,LOAD comprises
known DC load, including accessory loads.

Substituting equations for P.sub.A,ELEC and P.sub.B.ELEC, yields Eq. 4:
P.sub.BAT-(P.sub.A,MECH+P.subA^0SS)+(P.sub3,MECH+p.sub.B,L0SS)+P.sub.D- C
LOAD, [4]
wherein: P.sub.A,MECH comprises mechanical power from Motor A; P.sub.A,LOSS comprises
power losses from Motor A; P.sub.B.MECH comprises mechanical power from Motor B; and,
P.sub.B,LOSS comprises power losses . from Motor B.
Eq. 4 can be restated as Eq. 5, below, wherein speeds, N.sub.A and N.sub.B, and torques, T.sub.A
and T.sub.B, are substituted for power P.sub.A and P.sub.B. This includes an assumption that
motor and inverter losses can be mathematically modeled as a quadratic equation based upon
torque.
P.sub.BAT-(N.sub.AT.sub,A+'(a.sub.l(N.sub.A)T.sub.A+a,sub.2(N,sub.A)
T.sub.A+a.sub.SCN.sub.A^CN.sub.BT.sub.B+Cb.sub.l (N.sub.B)
T.sub.B.sup.2+b.sub.2(N.sub.B) T.sub.B+b.sub.3(N.sub.B)))+P.sub.DC LOAD [5]
wherein: N.sub.A, N.sub.B comprise speeds of Motors A, B;
T.sub.A, T.sub.B comprise torques of Motors A, B; and,
a.sub. 1, a.sub.2, a.sub.3, b.sub.l, b.sub.2, b.sub.3 each comprise quadratic coefficients which are
a function of respective motor speeds, N.sub.A, N.sub.B.
This can be restated as Eq. 6:
P.sub.B AT=a.sub. 1 *T.sub.A.sup.2-i-(N.sub. A+a.sub.2)*T.sub.A+b.sub. 1 *T.sub.B-
.sup.2+(N.sub.B+b.sub.2)*T.sub.B+a3+b3+P.sub.BAT.sub.-.sub.DC.sub.--.sub.- . LOAD [6]
This reduces to Eq. 7:
P.sub.B AT=a.sub-1. [T.sub-A.sup.2-HT.sub.A(N.sub. A+a.sub.2)/a.sub. l+((N.sub.r
A+a.sub.2)/2*a.sub.l).SLip.2]+b.sub.l[T.sub.B.si|p.2+T.sub.B(N.sub.B+b.sub.2-
)/b.sub. 1 +((N.sub.B+b.sub.2)/2*b.sub. 1 ).sup.2]

+a3*b3+P.su.b3AT.sub.--.subr.DC.SMb.".sub.LOAD"(N.syb.A+a,sub..2).SHp.?/(4*a,sub.l>
(N.sub.B+b.sub.2),s-yp.2/(4*b.sub.l) [7]
This reduces to Eq. §:
P.sub.B AT^sub. 1 [Trsub.A+(N.sub.A+a.sub.2)/(2*a.sub',;i"j].sup.2+b.sub. 1 [T.-
sub3+CN.sub.B^b.sub.2)/(2*b,sub.t)].sup.2+a.SLib,3+b.sub.3+P.sub.BAT.sub.-- T.sub.DC.sub,^
.sup,LQAD-(N.sub.A+a.sub.2).sup.2/(4'i,a.sub.l).(N.sub.B+b.su- b.2).sup.2/(4*b.sub.l) [8]
This reduces to Eq. 9:
P.sub.B AT-[SQRT(a.sub. I )*T,sub. A+(N.sub. A+a.sub.2).sup.2/(2*SQRT(a.sub. 1 )-
)].sup.2+[SQRT(b.sub.l)'i!T.sub.B+(N.sub.B+b,sub.2).sup.2/(2*SQRT(b.sub.!))]v 2
+a.sub.3+b.sub.3+P.sub.BAT.sub.--.sub.DC.sub.-.subXOAD-(N.sub.A+a.sub.-
2).sup.2/(4*a.sub.l)-CN.sub-B+b.sub.2),su.p.2/(4*b.sub.l) [9]
This reduces to Eq. 10:
P.sub.BAT=(A-Sub.l^T.sub.A+A.sub,2),sup.2+(B.sub,l*T.§ub.B+B.sub.2).sup.2^ +C . [10]
Wherein: A.sub.l=SQRT(a.sub.1) B.sub.l=SQRT(b.sub.l)
A2=(N.sub.A+a.sub.2)/(2*SQRT(a.sub,l)) B2=(N.sub,B+b.sub.2)/(2*SQRT(b.sub.l))
C=a.sub.3+b.sub.3+P.sub.BAT.sub.--.sub,DC.sub.-.sub.LOAD-(N.sub.A+a.sub.-
2).sup.2/(4*a.sub. 1 >(N.sub.B+b.sub.2).sup.2/(4*b..sub.l)
And, further reduceable to Eq. 11 and 12, below: PBAT=(TX.sup.?+TY.sup.2)+C [11]
P.sub.B AT=R.sup.2+C [12]
Eq. 12 yields the transformation of motor torque, T.sub. A to TX and a transformation of motor
torque T.sub, B to TY. The vector defined by TX/TY comprises battery power, P.sub.BAT.
Therefore, maximum ap.d minimum battery power, P.sub.B AT.sub.-^sub.MAX, and
P.sub.BAT.sub.-^.sub-MfN can be calculated and graphed as radii, Rmax ]24, and Rmin 122,
with a center at locus (0,0) in transformed space TX/TY,

as shown with reference to FIG. 3. Minimum and maximum battery power,
P.sub.BAT.sub.—.sub.M IN and P.sub.BAT.sub.—.sub.MAX, are preferably correlated to
various conditions, e.g. state of charge, temperature, voltage and usage (amp-hour/hour).
The parameter C. above, is defined as the absolute minimum possible battery power at
given speeds, N.sub.A, N.sub.B, ignoring motor torque limits.
Torque values Ta and Tb are transformable to TX and TY, as in Eq. 13:
##EQU000Q1##
wherein TX is the transformation of T,sub.A; TY is the transformation of T.sub.B; and,
A1, A2, Bl, B2 comprise scalar values. '
. The transformed vector [TX/TY] determined in Eq. 9 is solved simultaneously with the
torque space identified by R.sub.MIN 122 and R,sub.MAX 124, to identify motor torques
that are common to the first operating space and the second operating space, in TX/TY
space. The outcome of the solution is shown with reference again to FIG. 3, wherein
points A, B, C, D, and E represent the bounds for the common motor torques, in TX/TY
space. The various point? are defined as;
TABLE-US-00002 Point TX TY Radius or Line A TX.sup.A TY.sup.A Line B TX.sup.B
TY.sup.B Rmax C TX.sup.C TY.sup.C Line D TX.sup.D TY.sup.D Rmin E TX.sup^E
TY.sup.E Line

Because the equations are executed as algorithms'in TX/TY space, the execution time is
v ■:
effectively a single controller loop cycle, which can be in the range of 12 milliseconds or
less.
The resultant equations for common motor torques [TX/TY], defined by points A, B, C,
D, E are transformed again, to torques T.sub.A, T.sub.B of Motors A and B, calculable as
follows in Eq, 14:
##EQU00002##
The control system is operable to control operation of the transmission system within the
constraints of the range of operating points defined thusly. The algorithms constructed to
implement the equations described hereinabove are preferably regularly executed during
one of the aforementioned loop cycles to determine operating constraints of the electrical
motors A and B.
The invention has been described with specific reference to the preferred embodiments
and modifications thereto, Further modifications and alterations may occur to others upon
reading and understanding • the specificatipn. It is intended to include ajl such
modifications and alterations insofar as they come within the scope of the invention.

We Claim:
1. Method to determine a preferred operating range for a plurality of torque-
generative devices, each torque-generative device operable to provide motive
torque to a torque transmission device, comprising:
defining a first operating range in a first operating space;
defining a second operating range in the first operating space;
transforming the first operating range and the second operating range to a
second operating space; and,
defining the preferred operating range in the second operating space based upon
the transformed first operating range and the transformed second operating
range.
2. The method as claimed in claim 1, wherein defining the first operating range
comprises defining an operating range based upon torque output for each of the
torque-generative devices.
3. The method as claimed in claim 1, wherein defining the second operating
range comprises defining an operating range based upon output of an electrical
energy storage device operable to provide electrical energy to each of the
torque-generative devices.

4. The method as claimed in claim 3, wherein defining the operating range based
upon output of the electrical energy storage device comprises limited electrical
energy transmission to the electrical energy storage system to limit charging of
the electrical energy storage.
5. The method as claimed in elgim 3, wherein defining the operating range based
upon electrical energy system constraints comprises limiting electrical energy
transmission from the electrical energy storage system to limit discharging of the
electrical energy storage device.
6. The method as claimed in claim 1, wherein transforming the first operating
range and the second operating range to the second operating space comprises
linearly transforming the first operating range and the second operating range
from a radial dimention to an XY dimension,
7. The method as claimed in claim 1, comprising: retransforrning the defined
preferred operating ranp to the first operating space.
8. A system fpr control of a powertrain, the powertrain comprising an internal
combustion engine and a pair of electrical machines operably coupled to a two-
mode compound-split electro-mechanical transmission, the system comprising;
a plurality of electronic controllers signally interconnected via a local area
network and operable to control the engine and the transmission based upon
operator inputs determinable via a user interface; and

a storage device having a computer program encoded therein operable to
determine a preferred operating range for each of the eleptrical machines, the
system is configured to:
- define a first operating range in a first operating space;
- define a defining a second operating range in the first operating space;
- transform the first operating range and the second operating range to a second
operating space; and,
- define the preferred operating range in the second operating space based upon
the transformed first operating range and the transformed second operating
range.
9. The control system as claimed in claim 8, comprising:
means for retransforming the defined preferred operating range to the first
operating space.



ABSTRACT


TITLE: CONTROL SYSTEM FOR HYBRID POWERTRAIN
A method and apparatus for determining a preferred operating range for a plurality of
torque-generative devices is provided. Each device is operable to provide motive torque
to a transmission, The invention includes defining a first and a second operating range in
a first operating space. The first operating range and the second operating range are
mathematically transformed to a second operating space. The preferred operating range is
defined in the second operating space based upon the transformed first operating range
and the transformed second operating range. The first operating range is defined based
upon torque output for each of the torque-generative devices, The second operating range
is defined based upon output of an electrical energy storage device operable to provide
electrical energy to each of the torque-generative devices.

Documents:

01363-kol-2006 abstract.pdf

01363-kol-2006 claims.pdf

01363-kol-2006 correspondence others.pdf

01363-kol-2006 description(complete).pdf

01363-kol-2006 drawings.pdf

01363-kol-2006 form-1.pdf

01363-kol-2006 form-2.pdf

01363-kol-2006 form-3.pdf

01363-kol-2006 form-5.pdf

01363-kol-2006-assignment.pdf

01363-kol-2006-correspondence_1.1.pdf

01363-kol-2006-correspondence_1.2.pdf

01363-kol-2006-form-26.pdf

01363-kol-2006-priority document.pdf

1363-KOL-2006-(16-06-2014)-ABSTRACT.pdf

1363-KOL-2006-(16-06-2014)-ANNEXURE TO FORM 3.pdf

1363-KOL-2006-(16-06-2014)-CLAIMS.pdf

1363-KOL-2006-(16-06-2014)-CORRESPONDENCE.pdf

1363-KOL-2006-(16-06-2014)-DESCRIPTION (COMPLETE).pdf

1363-KOL-2006-(16-06-2014)-DRAWINGS.pdf

1363-KOL-2006-(16-06-2014)-FORM-1.pdf

1363-KOL-2006-(16-06-2014)-FORM-2.pdf

1363-KOL-2006-(16-06-2014)-PA.pdf

1363-KOL-2006-(16-06-2014)-PETITION UNDER RULE 137.pdf

1363-KOL-2006-(20-01-2012)-CORRESPONDENCE.pdf

1363-kol-2006-ASSIGNMENT.pdf

1363-kol-2006-CANCELLED PAGES.pdf

1363-kol-2006-CORRESPONDENCE.pdf

1363-kol-2006-EXAMINATION REPORT.pdf

1363-kol-2006-FORM 18-1.1.pdf

1363-kol-2006-form 18.pdf

1363-kol-2006-GPA.pdf

1363-kol-2006-GRANTED-ABSTRACT.pdf

1363-kol-2006-GRANTED-CLAIMS.pdf

1363-kol-2006-GRANTED-DESCRIPTION (COMPLETE).pdf

1363-kol-2006-GRANTED-DRAWINGS.pdf

1363-kol-2006-GRANTED-FORM 1.pdf

1363-kol-2006-GRANTED-FORM 2.pdf

1363-kol-2006-GRANTED-FORM 3.pdf

1363-kol-2006-GRANTED-FORM 5.pdf

1363-kol-2006-GRANTED-SPECIFICATION-COMPLETE.pdf

1363-kol-2006-OTHERS.pdf

1363-kol-2006-PETITION UNDER RULE 137.pdf

1363-kol-2006-REPLY TO EXAMINATION REPORT.pdf

1363-kol-2006-TRANSLATED COPY OF PRIORITY DOCUMENT.pdf

abstract-01363-kol-2006.jpg


Patent Number 265979
Indian Patent Application Number 1363/KOL/2006
PG Journal Number 13/2015
Publication Date 27-Mar-2015
Grant Date 26-Mar-2015
Date of Filing 15-Dec-2006
Name of Patentee GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Applicant Address 300 GM Renaissance CenterDetroit,Michigan 48265-3000
Inventors:
# Inventor's Name Inventor's Address
1 ANTHONY H. HEAP 2969 LESLIE PARK CIRCLEANN ARBOR,MICHIGAN 48105
PCT International Classification Number B60K17/28
PCT International Application Number N/A
PCT International Filing date
PCT Conventions:
# PCT Application Number Date of Convention Priority Country
1 11/352,771 2006-02-13 U.S.A.