Transcript of Lateral Stability Control of Electric Vehicle Based On ...
Microsoft Word - 29-06-019.docJ Electr Eng Technol Vol. 8, No. 4:
899-910, 2013 http://dx.doi.org/10.5370/JEET.2013.8.4.899
899
Lateral Stability Control of Electric Vehicle Based On Disturbance
Accommodating Kalman Filter using the Integration
of Single Antenna GPS Receiver and Yaw Rate Sensor
Binh-Minh Nguyen†, Yafei Wang**, Hiroshi Fujimoto* and Yoichi
Hori*
Abstract – This paper presents a novel lateral stability control
system for electric vehicle based on sideslip angle estimation
through Kalman filter using the integration of a single antenna GPS
receiver and yaw rate sensor. Using multi-rate measurements
including yaw rate and course angle, time-varying parameters
disappear from the measurement equation of the proposed Kalman
filter. Accurate sideslip angle estimation is achieved by treating
the combination of model uncertainties and external disturbances as
extended states. Active front steering and direct yaw moment are
integrated to manipulate sideslip angle and yaw rate of the
vehicle. Instead of decoupling control design method, a new control
scheme, “two-input two-output controller”, is proposed. The
extended states are utilized for disturbance rejection that
improves the robustness of lateral stability control system. The
effectiveness of the proposed methods is verified by computer
simulations and experiments.
Keywords: Electric vehicle, GPS, Lateral stability control, Kalman
filter
1. Introduction
The remarkable advantages of in-wheel motors have greatly improved
the motion control of electric vehicles (EVs) [1]. Firstly, torque
response of EV is very quick in comparison with that of internal
combustion engine vehicle. Secondly, yaw moment generated by
in-wheel motors can be used as a control input to the vehicle.
Finally, road condition is identified based on accurate motor
torque measurements. Lateral stability control is considered as one
of the critical issues in EV motion control. Yaw rate control alone
is inadequate for keeping the vehicle moving on low friction road
at high speed. Both yaw rate and sideslip angle must be controlled
to follow the reference values calculated from driver’s inputs [2].
While yaw rate can be measured using low cost gyroscopes, sideslip
angle sensors are very expensive for installation into commercial
vehicles. In order to keep the cost down while improving the safety
of EVs, the sideslip angle estimator plays an important role in
lateral stability control system.
Sideslip angle estimation methods can be categorized into three
groups: kinematic model-based estimation [3- 4], nonlinear dynamic
model-based estimation [5-6], and linear dynamic model-based
estimation [7-8]. Kinematic model based estimation does not rely on
the tire force characteristics of the vehicle. However, it uses
acceleration measurements which are always corrupted with
strong
noises. Moreover, roll angle and road inclination introduces offset
to lateral acceleration sensor signals due to gravity. Therefore,
kinematic model-based estimator cannot satisfy the requirement of
stability and robustness in long-term operation. Although nonlinear
observer has been developed theoretically, the nonlinear model is
complicated to implement in real time. On the other hand, linear
estimation using constant vehicle parameters is not robust enough
under the variation of road friction coefficient. In [9], adaptive
estimation of sideslip angle is proposed. However, the integration
of an observer with an online cornering stiffness identifier
increases the computational burden of the control system. The
accuracy of sideslip angle estimation relies on the accuracy of
cornering stiffness identification and vice versa. If the road
condition suddenly change (for instance, from high friction to low
friction), the sideslip angle estimation cannot be accurate until
the estimated cornering stiffness converge to the true values.
Therefore, it is essential to study the estimation methods that are
robust to the big change of road condition.
In recent years, robust estimation using nonconventional sensors
has been studied. Visual information can provide heading angle and
lateral distance of a vehicle for sideslip angle estimation [10].
However, visual signal may be unavailable when road markers are
covered with leaves, snow, water, or dirt. In [11], based on the
difference between the left and right tire lateral force
measurements, sideslip angle identification without cornering
stiffness is proposed. However, the high cost and the influence of
strong noises are big hurdles in using tire force sensors in
vehicle motion control.
Since the last decade, global positioning system (GPS)
† Corresponding Author: Dept. of Advanced Energy, the University of
Tokyo, Japan. (minh@hori.k.u-tokyo.ac.jp)
* Dept. of Advanced Energy, the University of Tokyo, Japan.
({fujimoto, hori}@k.u-tokyo.ac. jp)
** Dept. of Electrical Engineering, the University of Tokyo, Japan.
(wang@hori.k.u-tokyo.ac.jp)
Received: May 27, 2013; Accepted: June 7, 2013
ISSN(Print) 1975-0102 ISSN(Online) 2093-7423
Lateral Stability Control of Electric Vehicle Based On Disturbance
Accommodating Kalman Filter using the Integration of Single~
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has been a candidate for vehicle state estimation. The fusion of
GPS receiver with on-board dynamic sensors can provide accurate
state estimation in long-term operation. GPS can be used to measure
not only vehicle positions, but also velocity and attitude. By
using a double-antenna GPS receiver, sideslip angle can be
calculated directly [12]. A single-antenna GPS receiver can be
combined with a yaw rate sensor to estimate both sideslip angle and
yaw angle using a Kalman filter [13]. In [14], the integration of
single antenna GPS and a magnetometer introduces a new method for
sideslip angle estimation. Due to the poor update rate of GPS
receiver (1-10 Hz), the method proposed in [12] cannot satisfy the
requirement of advanced motion control of EVs in which the control
signals are generated every 1 millisecond. The fusion of GPS
receiver and yaw rate sensor in [13] can provide high-rate sideslip
angle estimation. However, the robustness of estimation under model
uncertainties and external disturbances was not examined. In [14],
the using of magnetometer increases the cost of this method.
Moreover, the methods proposed in [12-14] have not been integrated
with the controllers in real-time control system of vehicles.
In this paper, sideslip angle estimation based on a Kalman filter
that takes single-antenna GPS receiver and yaw rate sensor is
proposed. Following the idea of disturbance accommodating control
[15], by treating the model uncertainties and external disturbances
as extended states, high accuracy of estimation is achieved. An
important advantage of the proposed estimator is that yaw angle
(heading angle) can be estimated. The estimated yaw angle can be
used for other purposes, such as vehicle attitude control or
vehicle position estimation. Active front steering and direct yaw
moment are selected as control inputs for manipulating both yaw
rate and sideslip angle. Instead of decoupling control scheme, a
new “two-input two-output controller” is proposed. Using this
method, the decoupling term is unnecessary to be designed.
Therefore, the robustness of the decoupling term under the
variation of vehicle model is not a problem in this study. The
robustness of the system is also improved based on disturbance
estimation and rejection using Kalman filter.
β
γ
yu
Ti re
la te
Table 1. Nomenclatures
, f rl l Distances from front and rear axle to CG
, f rC C Front and rear cornering stiffness
zI Yaw moment of inertia
, f zNδ Front steering angle, yaw moment
M Vehicle mass , β γ Sideslip angle, yaw rate , ψ ν Yaw angle,
course angle from GPS ,x yu u
Longitudinal and lateral velocity
2. Vehicle Modeling The linear bicycle model shown in Fig. 1 is
constructed
under the following assumptions: 1) Tire slip angle is small so
that the lateral component of tire force is within linear region as
shown in Fig. 2. 2) Vehicle is symmetric about the fore-and-aft
center line. 3) Load transfer, roll motion, and pitch motion are
neglected.
During operation, external disturbances (lateral wind force, for
instance) frequently interfere with the vehicle system. The
influence of external disturbances can be generalized by lateral
force disturbance Fd and yaw moment disturbance Nd. The lateral
force equation and yaw moment equation can be expressed as
follows:
( ) 2 2f r x f f r d
x x
u u γ γ
(1)
2 2f r z f f f r r z d
x x
u u γ γ
γ β δ β = − + − + − + +
(2) Course angle of a moving vehicle is defined as the angle
between vehicle’s velocity vector and the geodetic North, as shown
in Fig. 1. Course angle is represented as the sum
Binh-Minh Nguyen, Yafei Wang, Hiroshi Fujimoto and Yoichi
Hori
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ν ψ β= + (3)
3. Experimental System A micro in-wheel motored EV named
“Super-capacitor
COMS” developed by EV team of Hori-Fujimoto Lab is used in this
study (Fig. 3). Two in-wheel motors are placed in the rear-left and
rear-right wheels. Thus, torque command can be distributed
independently to each wheel to generate a yaw moment. Active front
steering system is used as another control actuator which enables
the steer-by-wire mode. The vehicle is also equipped with a
gyroscope and accelerometers to measure yaw rate, longitudinal
acceleration, and lateral acceleration. In addition, a noncontact
optical sensor, Correvit (produced by Corrsys-Datron), is used for
accurate acquisition of vehicle sideslip angle, longitudinal
velocity, and lateral velocity. In this paper, it is used for
evaluating the performance of the proposed estimation algorithm.
Although it is placed at the front of the EV, sideslip angle at the
center of gravity can be derived based on the vehicle geometry with
the use of yaw rate measurement. Estimation and control algorithms
are implemented in a RT-Linux operating system computer which is
used as a main controller. The fundamental control period of the
system is 1 millisecond. The specifications of the experimental EV
are summarized in Table 2.
GPS receiver CCA-600 provided by Japan Radio Co. Ltd. is used in
this study. Table 3 shows the main features of CCA-600. It can
provide not only vehicle positioning but also velocity and course
angle. We design GPS software
with the following functions: 1) Decoding of the NMEA output
messages from CCA-600 and displaying the navigation data. 2)
Transferring of the motion measurement data to the main controller.
3) Recording the experimental data. The software is implemented in
a laptop to receive the NMEA messages from serial port, and then to
send the decoded data through LAN cable to EV’s controller.
A view of the GPS software’s interface is shown in Fig. 4. Using
the software we can receive the GPS receiver’s dilution of
precision (DOP), the detailed information of satellites in view
like carrier-to-noise ratio (CNR). Such kind of information is
essential for evaluating the accuracy of GPS measurement in real
time. Fig. 4 also shows the vehicle positions on Google Earth,
vehicle velocity and course angle obtained from an experiment. The
software can also transfer the position on longitude-latitude
coordinates to the planar North-East coordinates and calculate the
driving distance of the vehicle.
Fig. 4. GPS software interface and experimental data
CCA-600 antenna
Lateral Stability Control of Electric Vehicle Based On Disturbance
Accommodating Kalman Filter using the Integration of Single~
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Total mass 400 kg Wheel base 1.2 m
Track-width of rear wheel 0.82 m Height of CG 0.4 m Wheel radius
0.26 m
Wheel spin inertia 1.26 kgm2 Yaw moment of inertia 136 kgm2
Energy store (super-capacitor) 210V, 29F, 173 Wh Main controller
PC104, Linux OS
In-wheel motor type PMSM Max. motor power 2 kW Max. motor torque
100 Nm
Max. vehicle velocity 50 km/h
Table 3. Features of GPS receiver CCA-600
Receiving method L1(1575.42 MHz)GPS (C/A) Augmentation method
Satellite based (SBAS) Positioning accuracy 2.5 m CEP
Course angle accuracy 0.14 degree RMS Velocity accuracy 0.05 m/s
RMS
Data format NMEA-0183 Current consumption 36 mA
Update rate 5 Hz
4.1 Disturbance accommodating dynamic model Basically, the
estimation model is designed using
nominal values of cornering stiffness: Cfn and Crn. Due to the
change of road condition, the nominal cornering stiffness differs
from the true values. The variation of tire cornering stiffness can
be expressed by the following equations:
f fn f
r rn r
= + Δ = + Δ
From (1)-(4), a state space model of vehicle dynamics
can be derived as (5)-(10) in which the unknown input disturbance
d1 and d2 represent the combined influence of external disturbances
and cornering stiffness variation. The input vector u includes the
front steering angle and yaw moment generated by in-wheel motors
and w is the process noise vector. In (7), an11, .., an22, bn11, …,
bn22 are calculated using the nominal vehicle parameters (detailed
formulation are presented in the Appendix).
n n nx A x B u D wς= + + + (5)
[ ] [ ]1 2, , TT T
f zx u N d dβ γ ψ δ ς = = = (6)
11 12 11 12
21 22 21 22
0 1 0 0 0 0 0
n n n n
n n n n n n n
= = =
x x
Mu Mu C
F Mu Mu
z z x
I I u C l
N I I
The continuous time model (5) is transformed to the
discrete time model (10) by using the transformation (11) in which
Tc is the fundamental sampling time (1 millisecond in this
paper).
1k nd k nd k nd k kx A x B u D wς+ = + + + (10)
0 0
, , c c
T T A T A A
nd nd n nd nA e B e d B D e d Dτ ττ τ= = =∫ ∫ (11)
In [15], disturbance accommodating control was firstly
introduced to control theory. The original idea is that the
external disturbances can be augmented to be extended states. In
this paper, this idea is applied in Kalman filter for sideslip
angle estimation by assuming the unknown input terms can be
considered as stochastic processes with zero- mean white noise
sequence:
1 ,k k dis kwς ς+ = + (12)
Based on the assumption (12), a new state space model
is constructed as follows:
,
dis kk
wς
, 0 [ ] 0
I ×× ×
where [I] represents the identity matrix, and [0]
represents the zero matrix. Wk is the process noise vector of the
disturbance accommodating system at step k.
4.2 Multi-rate output measurements
In the Kalman filter algorithm, output measurement is
used for the correction stage. If lateral acceleration is selected
as measurement, the output measurement equation is expressed as
follows:
( ) ( )2 2 2 2f r r r f f y
x
M Mu β γ
903
, ,
T
k nd k k gyro k GPS kY C X V γ ν = + = (17)
0 1 0 0 0 course angle update
1 0 1 0 0
0 1 0 0 0 during inter-samples
0 0 0 0 0
nd
nd
C
C
(18)
In (17), Vk is the measurement noise vector at step k.
Output measurement equation (17) does not rely on tire cornering
stiffness. This is the advantage of using course angle in sideslip
angle estimation. The observability of sideslip angle and
disturbance terms are assured by checking the rank of matrix 4
T
nd nd nd nd ndC C A C A . If the GPS signal is unavailable,
accurate yaw angle estimation is impossible. Even though, sideslip
angle and the disturbance terms can be estimated using only yaw
rate sensor. Therefore, lateral stability control can be realized
in case that GPS signal is lost.
4.3 Noise covariance matrices
QW and RV are process noise and measurement noise
covariance matrices, respectively. QW represents the accuracy of
dynamical model and RV shows the level of confidence placed in
sensor measurements. In principle, the covariance matrices are not
necessarily diagonal. In order to reduce the computational time
when implementing the algorithm in the real-time control system, QW
and RV are treated as diagonal matrices as follows:
1 2 diag , , , ,W d dQ Q Q Q Q Qβ γ ψ = (19)
diag ,VR R Rγ ν = (20) If RV is set too large, the Kalman gain will
decrease, thus,
the estimation fails to update the propagated disturbances based on
measurements. On the other hand, small QW results in unstable
estimation, while large QW will force the
estimation to completely rely upon the measurements, leading to
measurement noise being directly transmitted into the estimated
states. While Rγ is almost constant, Rν relies on the working
condition of GPS receiver. According to GPS technology, the
relative satellite-receiver geometry plays an important role in
accuracy of positioning. Rν can be adjusted in real-time based on
the dilution of precision of the GPS receiver. This problem will be
addressed in future works. In this paper, trial-and-error method
was conducted to select the suitable noise covariance
matrices.
4.4 Kalman filter algorithm
two stages:
2) Correction based on multi-rate measurements. Therefore, the
algorithm is named disturbance accommodating multi-rate Kalman
filter (DAMRKF) in this paper.
1k nd k nd kX A X B U+ = +
1 T
( ) 1
1 1 1 T T
+ + += +
( )1 1 1 1 1 ˆ
k k k k nd kX X L Y C X+ + + + += + −
1 1 1k k nd kP I L C M+ + + = −
0 0 ˆ( , )X P
Fig. 5. Kalman filter algorithm
5. Lateral Stability Control Design In this section, lateral
stability control system of in-
wheel motored electric vehicle is proposed. The general control
system is shown in Fig. 6, and can be summarized as follows.
1) The reference model is obtained from the linear bicycle
model.
2) The DAMRKF designed in the previous section provides the
estimated values of sideslip angle, yaw rate and the disturbance
terms that incorporate model error and external disturbances.
3) The purpose of the lateral stability control is to make the
vehicle follow the desired trajectory. The system has two layers.
In the upper layer, a new control
Lateral Stability Control of Electric Vehicle Based On Disturbance
Accommodating Kalman Filter using the Integration of Single~
904
scheme is proposed for yaw rate and sideslip angle tracking. In
order to guarantee the robustness of the system, the upper layer is
designed as a combination of 2-DOF control configuration and
disturbance rejection. The upper layer outputs the yaw moment
command and front steering angle commands to the lower layer
including electric power steering control (EPSC) and the motor
torque distribution (MTD).
5.1 Reference model
The reference model is determined based on the steady
( ) ( )
x f r
β δ
u Gu l l
− =
In [8], both yaw rate and sideslip angle are controlled
only by yaw moment generated by the in-wheel motors. Therefore,
there is a “trade-off” between sideslip angle control and yaw rate
control. In [11, 16], and [17], active front steering is integrated
with direct yaw moment control by different schemes. In [11],
decoupling control method is utilized such that sideslip angle is
controlled by front steering angle and yaw rate is controlled by
yaw moment. It means the decoupling terms are designed in the upper
control layer. As discussed in [16] and [17], the decoupling
control is not robust enough under the variation of cornering
stiffness. In case of big cornering stiffness error, i.e., 30% of
the true value, the state responses will have a
terrible oscillation about the desired values. Based on disturbance
observer theory, in [16] and [17], a new decoupling control scheme
is proposed with high robustness under model error. This scheme is
a combination of yaw moment observer and lateral force observer
that can compensate the lumped disturbances and nominalize the
system as follows:
1
2
Accurate sideslip angle is essential for lateral force
observer. However, the problem of sideslip angle estimation was not
solved in [16-17]. In this paper, we aim to propose a control
scheme that can achieve two goals simultaneously: robust estimation
of sideslip angle and robust lateral stability control. Thanks to
the DAMRKF, sideslip angle and disturbance terms are estimated.
While the estimated sideslip angle can be used for the 2-DOF
control design, the estimated disturbance terms can be used to
compensate the influence of model error. Moreover, it is
unnecessary to decouple the two control inputs. Considering the
controlled states as a vector of two components, model following
control can be applied for obtaining the input vector.
Design of disturbance rejection
The dynamics of the lateral motion can be expressed as
follows:
11 12 11 12 1
21 22 21 22 2
n n n n f
n n n n z
a a b b d a a b b N d
δββ γγ
disturbance rejection matrix is designed as follows:
1
Fig. 6. Lateral stability control system based on disturbance
accommodating multi-rate Kalman filter
Binh-Minh Nguyen, Yafei Wang, Hiroshi Fujimoto and Yoichi
Hori
905
With the disturbance rejection, the vehicle system’s behavior is
augmented to be the nominal model. Therefore, the robustness of the
control system is improved. The feed- back and feed-forward
controller are designed based on the nominal model for the tracking
purpose.
Design of feed-forward controller
From (25), the transfer function from the control input vector to
the controlled state vector is derived as follows:
1
21 22 21 22
n n n n
a a b b
The detailed formulation of Pn is presented in the
Appendix. The feed forward controller is designed as the inverse of
Pn given by:
11 121
21 22
Design of feed-back controller
The desired closed loop system including the feed-back controller
and the plant is expressed as follows:
0
0
In (29), the cut-off frequency Kβ and Kγ were determined
( )
( )
C C C P K I K
C C
The feedback controller augments the closed loop
system to the desired model K with the poles placed at -Kβ and -Kγ.
The internal stability of the system is assured by verifying the
poles of the following matrices of transfer function:
( ) ( ) ( )1 1 11 and n n fb n fb n fb n fb n fbP I P C P C P C I P
C P C − − −− + +
Finally, the control commands are obtained as follows:
*
dz d
− = + − −
Yaw moment is generated by the difference between the
*
z
d T T N
(32)
where r is the wheel radius, Tcmd is the torque command given by
the driver, and dr is the track-width between two rear wheels.
m
RLT and m RRT are the rear-left and rear-right
in-wheel motor’s torque, respectively. An EPS motor is utilized for
generating the front
steering angle (Fig. 7). This system enables the steer-by- wire
mode for manipulating the vehicle without the driver’s
handling.
Fig. 7. Front EPS motor system
6. Simulation Results Based on the vehicle specification in Table
II, vehicle
model was constructed using Matlab/Simulink. The sampling time of
simulation is set to 1 millisecond to match that of the experiment
condition.
6.1 Sideslip angle estimation results
In this simulation, we verify the proposed Kalman filter
in comparison with other estimation methods. Two cases of driving
are simulated: cornering test and lane-change test with sinusoidal
steer command. In both cases, the following driving conditions were
set:
1) The longitudinal velocity is 25 km/h. 2) From 4 second, a strong
lateral wind force starts to act
on the vehicle. It introduces lateral force disturbance Fd
Lateral Stability Control of Electric Vehicle Based On Disturbance
Accommodating Kalman Filter using the Integration of Single~
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and yaw moment disturbance Nd. 3) The cornering stiffness of
vehicle model are Cf = Cr =
7000 N/rad. However, the estimation model is designed with the
nominal values Cfn= Crn=10,000 N/rad. This means a big error is
introduced to cornering stiffness of the estimation model.
4) The disturbance terms d1 and d2 are simulated using (8) and
(9).
5) The DAMRKF is compared to the following two methods. The first
is the sideslip angle estimation using linear observer (LOB) with
constant cornering stiffness model, as described in [8]. Yaw rate
and lateral acceleration are selected as output measurements. The
second method is multi-rate Kalman filter (MRKF) proposed in [13].
This method uses the yaw rate and course angle as output
measurement.
Simulation results of two tests, cornering test and lane
change test, are shown in Fig. 8 and Fig. 9, respectively. The
results include sideslip angle estimations and disturbance
estimations. The influence of lateral wind force can be
demonstrated by the change of sideslip angle and disturbance terms
from 4 second. In both tests, LOB shows the poorest estimation
performance. By using course angle from GPS, MRKF provides better
estimation than LOB. However, the results degrade under the
influence of both model error and lateral wind force. By using the
proposed DAMRKF method, the disturbances are estimated as the
extended states. Although the tracking of disturbance
estimation is not perfect, sideslip angle estimation performance is
improved considerably. Therefore, the assumption of the dynamics of
disturbances in (12) is acceptable.
6.2 Lateral Stability Control Results
After evaluating the estimation algorithm, the
Matlab/Simulink model of the whole system in Fig. 6 is constructed.
Fig. 10 demonstrates vehicle motion with step steer command. The
simulation conditions were set the same as the previous sub-section
(under model error and lateral wind force). In the case of without
lateral stability control, vehicle motion is handled by only
driver’s steer command. In this case, both the yaw rate and the
side slip angle increases considerably in comparison with the
desired values. In contrast, with the proposed control system,
active front steering and yaw moment are generated to control the
sideslip angle and the yaw rate to follow their desired
values.
7. Experimental Results
7.1 Sideslip angle estimation results Before implementing the
control algorithm, experiments
were conducted with driver’s command input only. Based on the
experimental results, trial-and-error method was
1 2 3 4 5 6 7 -0.01
0
0.01
0.02
0.03
0.04
0
0.05
0.1
0.15
0.2
-0.2
0
0.2
0.4
0.6
True value DAMRKF
(a) (b) (c)
Fig. 8. Simulation results of sideslip angle estimation: Cornering
test. (a) Sideslip angle; (b). Disturbance term d1; (c).
Disturbance term d2.
1 2 3 4 5 6 7 -0.05
0
0.05
-0.2
-0.1
0
0.1
0.2
-0.4
-0.2
0
0.2
0.4
0.6
(a) (b) (c)
Fig. 9. Simulation results of sideslip angle estimation:
Lane-change test. (a) Sideslip angle; (b). Disturbance term d1;
(c). Disturbance term d2.
Binh-Minh Nguyen, Yafei Wang, Hiroshi Fujimoto and Yoichi
Hori
907
used to select the suitable noise covariance matrices for Kalman
filter design. Like the simulation, the nominal cornering stiffness
of the estimation model is set as Cfn = Crn = 10,000 N/rad. The
cornering stiffness according to road condition is approximately Cf
= Cr ≈ 7000 N/rad. The velocity of vehicle on this test is
controlled at about 20 km/h. During the test, wind force introduced
the unknown input disturbances to the estimation system. Sideslip
angle estimation results are shown in Fig. 11 (a). As the
simulation, LOB has largest estimation error in comparison with the
sideslip angle obtained from optical sensor. MRKF is shown to be
superior, but it is still sensitive to model errors and
disturbances. The proposed DAMRKF, on the other hand, is robust to
both model errors and
disturbances. The disturbance terms estimated by this method are
shown in Figs. 11 (b-c). Fig. 11 (d) shows the course angle
measured by GPS receiver and the estimated yaw angle by DAMRKF.
While yaw angle was estimated every 1 millisecond, the sampling
time of course angle from GPS was 200 milliseconds. This is another
advantage of the proposed DAMRKF.
7.2 Lateral stability control results
In this sub-section, results of cornering test are shown.
Instead of handling by the driver, steer-by-wire mode is used for
generating front steering angle. The steering command is
pre-designed and generated by the program.
1 2 3 4 5 6 7 -0.01
0
0.01
0.02
0.03
0.04
-0.6
-0.4
-0.2
0
0.2
-0.08
-0.06
-0.04
-0.02
0
0.02
-200
-100
0
100
200
300
(a) (b) (c) (d)
Fig. 10. Simulation results of lateral stability control based on
DAMRKF: Cornering test. (a) Sideslip angle; (b). Yaw rate (c);
Front steering angle; (d). Yaw moment.
4 5 6 7 8 9 10 11 12 13 14 -0.06
-0.04
-0.02
0
0.02
0.04
0.06
DAMRKF
4 5 6 7 8 9 10 11 12 13 14
-0.2
-0.1
0
0.1
0.2
0.3
d1 (DAMRKF)
(a) (b)
4 5 6 7 8 9 10 11 12 13 14 -0.3
-0.2
-0.1
0
0.1
0.2
0.3
0.4
d2 (DAMRKF)
4 5 6 7 8 9 10 11 12 13 14 3.8
3.9
4
4.1
4.2
4.3
4.4
4.5
4.6
4.7
(c) (d)
Fig. 11. Experiment results of sideslip angle estimation:
Lane-change test. (a) Sideslip angle; (b) Disturbance term d1; (c)
Disturbance term d2; (d) Course angle.
Lateral Stability Control of Electric Vehicle Based On Disturbance
Accommodating Kalman Filter using the Integration of Single~
908
The velocity of vehicle in this experiment is 18 km/h. By this way,
the same driving condition is made for the cases of with stability
control and without stability control. Fig. 12 shows that, in case
of without control, both sideslip angle and yaw rate increases over
the desired values. When the proposed control system was applied,
sideslip angle and yaw rate follows the reference model. This means
that the stability of the EV is improved.
8. Conclusions The most important contribution of this paper is a
new
method for robust estimation of sideslip angle using a single
antenna GPS receiver and yaw rate sensor. By applying the
disturbance accommodating idea, accurate estimation was achieved
even under model error and external disturbance. The effectiveness
of the proposed DAMRKF was demonstrated by both simulations and
experiments. Moreover, DAMRKF was successfully implemented in a
lateral stability control system of electric vehicle with rear
in-wheel motors and front active steering. Based on the DAMRKF, a
new scheme for combining front steering and yaw moment control was
proposed. It is a combination of 2-DOF control and disturbance
rejection. DAMRKF kills two birds with one stone by providing not
only accurate state estimates but also disturbance estimates for
improving control robustness. However, the following questions
still remain: 1) How to improve the multi-rate estimation because
during inter-samples there are no new updates of measurement based
on GPS. 2) How to tune the noise covariance according to GPS
measurement in real time. These problems will be solved in future
works to fulfill the algorithm of vehicle state estimation using
GPS.
Acknowledgements The authors would like to thank Japan Radio Co.
Ltd.
for supporting GPS receiver CCA-600.
Appendix: Lateral Dynamic Derivation The components of the matrices
that represent lateral
dynamic motion are calculated as follows:
( ) ( )
xn n x
n n fn f rn r fn f rn r
z z x
C l C lC C Mua a Mu
−− + − −
= − − − +
=
11 21 12 11 22 11
11 22 12 21
11 22 12 21
22 22 11 22
11 22 12 21
n n n n
n n n n
n n n n
n n n n
s a s a a a b a
P s a s a a a b s b a b a
P s a s a a a
b s b a P
s a s a a a
+ − = − − − = − − − + − = − − − − =
− − −
controllers are expressed as follows:
( )
( )
( )
11 22
11 22
n n
n n
b b a
b b b s b a b a
C b b
0
0.01
0.02
0.03
0.04
-0.4
-0.2
0
0.2
0
0.01
0.02
0.03
0.04
-0.3
-0.2
-0.1
0
0.1
(a) (b) (c) (d)
Fig. 12. Experiment results of lateral stability control based on
DAMRKF: Cornering test.: (a) Sideslip angle (without control); (b)
Yaw rate (without control); (c) Sideslip angle (with control); (d)
Yaw rate (with control).
Binh-Minh Nguyen, Yafei Wang, Hiroshi Fujimoto and Yoichi
Hori
909
11 22
11 22
n n
n n
b b s s K
a s K K C
b s s K
b s b a b a s K K C
b b s s K
b s b a b a s K K C
b b s s K
γ β
(37)
References
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Binh Minh Nguyen was born in Haiphong, Vietnam. He is currently
working toward the Ph.D. degree in the Department of Advanced
Energy, Graduate School of Frontier Sciences, the University of
Tokyo. His current research interests include robust con- trol
theory, sensor fusion, motion control
of electric vehicle, visual servo system.
Yafei Wang received the Ph.D. degree in Electrical Engineering from
the University of Tokyo, Tokyo, Japan, in 2013. From 2008 to 2010,
he worked in automotive industry for nearly 2 years, including
internships with Cat- erpillar Remanufacturing Services (Shanghai)
and FIAT Powertrain Tech-
nologies (Shanghai), and full-time experience with Delphi China
Technical Center (Shanghai). Currently, he is working as a
postdoctoral researcher in the University of Tokyo. He is
interested in state estimation and motion control for electric
vehicles, multi-rate estimation theory, and real-time image
processing.
Lateral Stability Control of Electric Vehicle Based On Disturbance
Accommodating Kalman Filter using the Integration of Single~
910
Hiroshi Fujimoto received the Ph.D. degree from The University of
Tokyo, Tokyo, Japan, in 2001. In 2001, he joined the Department of
Electrical Engineering, Nagaoka University of Technology, Niigata,
Japan, as a Research Associate. From 2002 to 2003, he was a
Visiting Scholar with
the School of Mechanical Engineering, Purdue University, West
Lafayette, IN. In 2004, he joined the Department of Electrical and
Computer Engineering, Yokohama National University, Yokohama,
Japan, as a Lecturer, and he became an Associate Professor in 2005.
He has been an Associate Professor with the Department of Advanced
Energy, Graduate School of Frontier Sciences, The University of
Tokyo, since 2010. His research interests include control
engineering, motion control, nanoscale servo systems, electric
vehicle control, and motor drives. Dr. Fujimoto is a Member of the
Institute of Electrical Engineers of Japan, the Society of
Instrument and Control Engineers (SICE), the Robotics Society of
Japan, and the Society of Automotive Engineers of Japan. He
received the Best Paper Award from the IEEE TRANSACTION ON
INDUSTRIAL ELECTRONICS in 2001, the Isao Takahashi Power
Electronics Award in 2010, and the Best Author Prize from the SICE
in 2010.
Yoichi Hori received the B.S., M.S., and Ph.D. degrees in
electrical engine- eering from The University of Tokyo, Tokyo,
Japan, in 1978, 1980, and 1983, respectively. In 1983, he joined
the Department of Electrical Engineering, the University of Tokyo,
as a Research Associate, where he later became an
Assistant Professor, an Associate Professor, and, in 2000, a
Professor. He moved to the Institute of Industrial Science as a
Professor with the Information and System Division in 2002 and to
the Department of Advanced Energy, Graduate School of Frontier
Sciences, The University of Tokyo, in 2008. From 1991 to 1992, he
was a Visiting Researcher with the University of California,
Berkeley. His research interests are control theory and its
industrial applications to motion control, mechatronics, robotics,
electric vehicles, etc. Dr. Hori has been the Treasurer of the IEEE
Japan Council and Tokyo Section since 2001. He is also an
Administrative Committee member of the IEEE Industrial Electronics
Society and a member of the Society of Instrument and Control
Engineers, the Robotics Society of Japan, the Japan Society of
Mechanical Engineers, and the Society of Automotive Engineers of
Japan (JSAE). He was the President of the Industry Applications
Society of the Institute of Electrical Engineers of Japan (IEEJ),
the President of Capacitors Forum, the Chairman of the Motor
Technology Symposium of the Japan Management Associ- ation, and the
Director on Technological Development of JSAE. He received the Best
Transactions Paper Award from the IEEE TRANSACTION ON INDUSTRIAL
ELECTRONICS in 1993 and 2001, the 2000 Best Transactions Paper
Award from the IEEJ, and the 2011 Achievement Award from the
IEEJ.
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<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>
/SVE
<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>
/CHS
<FEFF4f7f75288fd94e9b8bbe7f6e521b5efa76840020005000440046002065876863ff0c5c065305542b66f49ad8768456fe50cf52068fa87387ff0c4ee575284e8e9ad88d2891cf76845370524d6253537030028be5002000500044004600206587686353ef4ee54f7f752800200020004100630072006f00620061007400204e0e002000520065006100640065007200200035002e00300020548c66f49ad87248672c62535f0030028fd94e9b8bbe7f6e89816c425d4c51655b574f533002>
/CHT
<FEFF4f7f752890194e9b8a2d5b9a5efa7acb76840020005000440046002065874ef65305542b8f039ad876845f7150cf89e367905ea6ff0c9069752865bc9ad854c18cea76845370524d521753703002005000440046002065874ef653ef4ee54f7f75280020004100630072006f0062006100740020548c002000520065006100640065007200200035002e0030002053ca66f465b07248672c4f86958b555f300290194e9b8a2d5b9a89816c425d4c51655b57578b3002>
/KOR
<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>
>> >> setdistillerparams << /HWResolution [2400
2400] /PageSize [545.000 394.000] >> setpagedevice