This application claims priority of French application No. 05 53787 filed Dec. 8, 2005, which is incorporated by reference herein in its entirety.
The invention concerns a method for estimating in real time on a vehicle in motion a front transverse force applied by the ground to the front wheels, and a rear transverse force applied by the ground to the rear wheels of this vehicle.
The forces transmitted by the ground to a wheel of the vehicle can be decomposed along three directions. As illustrated on
Improving the comfort and the active safety requires knowing in real time the longitudinal and transverse forces of the front wheels and of the rear wheels. Knowing them makes it possible, for example, to monitor the position, the speed, and the acceleration of the vehicle, and, more generally, the behavior of this vehicle by acting on driven components such as the brakes, the engine, the active steering, or the suspensions.
However, the longitudinal and transverse forces cannot be measured in real time in a direct way at a cost compatible with the mass production of a high number of vehicles. Therefore, indirect methods are used, for example, consisting in regulating another variable that can be measured in real time.
This other variable is, for example, the transverse position of the upper portions of the wheels which is representative of their camber angle; the transverse acceleration of the vehicle; the yaw rate of the vehicle, i.e., its rotation speed about a vertical axis; or the angle of the steering wheel.
These indirect methods are satisfactory for the longitudinal dynamics, but not for the transverse forces.
The estimation of the transverse forces can be performed with open-loop estimation methods using various measurements in association with a model of the tire.
However, the transverse forces are a function of the drifts of the tires, of the steering and camber angles of the wheels, and of the load on each wheel. In addition, the drifts of the tires depend for their part on the longitudinal and transverse velocities of the vehicle as well as on the position of the center of gravity of the vehicle, so that the open-loop estimation methods are not sufficiently reliable.
The goal of the invention is to propose a method that makes it possible to estimate the transverse forces in real time in a reliable manner.
To this effect, an object of the invention is a method for estimating in real time, in a motor vehicle, a front force and a rear force, these forces being applied by the ground to the front wheels and to the rear wheels, respectively, of the vehicle along a transverse direction, this method consisting in:
According to a characteristic of the invention, the processing operation includes a feedback loop, and implements a dynamic model that makes it possible to determine a transverse acceleration and a yaw rate from a front force and a rear force, and consists in:
According to another characteristic of the invention:
According to another characteristic of the invention, the method is discretized, and consists in determining a new estimated front force value and a new estimated rear force value, from new transverse acceleration and yaw rate measurements, and from current values of estimated front force and estimated rear force, and by actualization and correction of intermediary values of front and rear forces, consisting in:
The invention also concerns a method for estimating, in a vehicle and in real time, a transverse force applied by the ground to each wheel, consisting in:
As a variant, the invention also concerns a method for estimating, in a vehicle and in real time, a transverse force applied by the ground to each wheel, consisting in:
According to a first characteristic, the above-defined method consists in:
According to this first characteristic, the estimation device implements the following equations:
with
a and b, the front and rear wheel bases, respectively,
E=a+b is the total wheel base,
v is half the distance between the left and right wheels of the vehicle,
h: height of the center of gravity G of the vehicle with respect to the ground,
m: mass of the vehicle,
g: acceleration of gravity,
γx and γT: longitudinal and transversal accelerations, respectively, of the vehicle considered at the center of gravity G
According to another characteristic of this variant, the method consists in:
According to this other characteristic, the estimating device comprises a mechanical model of the vehicle receiving as a first series of inputs, the longitudinal velocity, the longitudinal and transverse accelerations, the yaw rate, the vertical velocity, the roll rate, and the pitch rate, respectively, and receiving as a second series of inputs, the estimated vertical forces applied by the ground to the pneumatic tires of the left front wheel, right front wheel, left rear wheel, and right rear wheel, respectively ; these forces corresponding to the outputs of determined transfer functions specific to each wheel, respectively, these transfer functions receiving at their respective inputs, the discrepancy between the wheel displacements measured by measuring devices adapted to supply signals representative of said displacements, respectively, and the displacements of the wheels estimated by the model.
The invention will now be described in more details, and in reference to the annexed drawings which illustrate an embodiment thereof by way of a non-limitative example.
The invention concerns a closed-loop method for estimating in real time the inputs of a system which is a motor vehicle, the estimated inputs being the front and rear transverse forces.
The closed-loop estimation methods, also known under the name “observer,” make it possible to estimate state variables such as the position, the angle, the velocity, the acceleration, by using a dynamic mechanical model driven by a feedback loop depending on the estimation error.
The method according to the invention applies to a modeled physical system under the following form:
in which:
t: time
X: state variables;
U: input/control variables;
Y: output/measurement variables;
The variables X, U, and Y are vectors, having dimensions m, n, and p, respectively. A, B, and C are constant matrices representative of the physical system under consideration.
The idea at the basis of the invention is to estimate the components of the vector U, whose estimation is noted Ue, while the transfer function connecting the input of the system to its output is designated by T(s). Thus, we have:
in which s is the Laplace variable, and I is the identity matrix.
By noting
the transfer function that it is desired to have between the input to be estimated U and the estimated input Ue, the estimation of the input is given by the equation Ue(s)=L(s)(Y(s)−Ye(s)) in which L is a gain matrix defined by the transfer function L(s)=Gd(s)(I−Gd(s))31 1T−1(s),
Ye(s) is the estimation of the measurements, obtained by the following equation:
Then, Ue tends towards U, i.e., limt→∞∥U(t)−Ue(t)∥=0 in an asymptotic manner, when various conditions are verified, i.e., the fact that the matrix T is reversible, that Gd is adapted to make L causal, and that the matrices A, B, and C are sufficiently full.
According to the invention, the estimation of the transverse forces is performed by applying to the vehicle a simplified dynamic mechanical model, such as a model of the tireless bicycle type, like the one that is shown schematically on
The front transverse force FyF is applied by the ground to the front wheel of the bicycle model, it corresponds to the sum of the transverse forces applied to the two front wheels of the vehicle. In an analogous manner, the rear transverse force FyR corresponds to the sum of the forces applied to the rear wheels of the vehicle.
As shown schematically on
The vehicle moves longitudinally at a velocity noted Vx, it has a transverse velocity noted Vy, it is moving with a velocity called yaw rate, noted Vψ and corresponding to its rotation speed about a vertical axis.
The equations of the vehicle according to the tireless bicycle dynamic model are given below:
The transverse velocity is not measured directly, but measurements of the yaw rate V104 and of the transverse acceleration γt={dot over (V)}y−VxVψ are available, these measurements stemming from one or several devices including, for example, two dedicated acceleration sensors.
This makes it possible to rewrite the model as follows:
The matrix connecting
is then:
The transfer function Gd(s) connecting the input to be estimated U and the estimated input Ue can be chosen as being
given that the choice of this transfer function is free. τ is a time constant, i.e., representative of the reaction time of the system, and its value is, for example, 1/100th of a second.
The estimated input Ue is then given by the following expression:
in which
As illustrated by
The method is also shown on
This processing unit is connected in particular to one or several measuring devices supplying a signal representative of the transverse acceleration γT and a signal representative of the yaw rate Vψ.
This processing operation implements a dynamic model, represented by the block B1, which is exploited by feedback to a regulator represented by the block B2. The regulator B2 receives as input discrepancies between measured and estimated values of transverse acceleration and yaw rate, and it supplies as output the front force and the rear force. The dynamic model of the block B1 receives as input the output of the regulator to supply as output an estimated transverse acceleration and an estimated yaw rate, which are injected into the discrepancies applied at the input of the regulator B2.
More particularly, the dynamic mechanical model of the tireless bicycle type, represented by the block B1, receives as input values or signals representative of the estimated front transverse force FyFe and of the estimated rear transverse force FyRe to supply as output values or signals representative of an estimated transverse acceleration γTe and of an estimated yaw rate Vψe.
As shown schematically in the block B1, the yaw rate is determined by integration of the moment of the front force FyFe and of the rear force FyRe about a vertical axis coinciding with the measuring device. The transverse acceleration γTe, for its part, results from the sum of the front and rear forces divided by the mass of the vehicle.
The regulator represented by the block B2 receives as input a first discrepancy signal and a second discrepancy signal to supply as output signals representative of the estimated front force FyFe and of the estimated rear force FyRe.
The first discrepancy is representative of the difference between the measured acceleration γT, i.e., stemming from the measuring device, and the estimated acceleration γTe resulting from the dynamic model, i.e., stemming from the block B1.
The second discrepancy is representative of the difference between the measured yaw rate V104 , i.e., stemming from the measuring device, and the estimated yaw rate V104 , i.e., stemming from the dynamic model of the block B1.
As shown schematically in the block B2, the first discrepancy and the second discrepancy applied as input of the regulator B2 are processed by performing a processing operation of the proportional and/or integral type to generate as output signals or values representative of the estimated front force FyFe and of the estimated rear force FyRe.
More particularly, the signal representative of the front transverse force FyFe is obtained by applying a proportional integral processing operation to the first discrepancy, by applying a proportional processing operation to the second discrepancy, and by combination of the thus generated signals.
The signal representative of the rear transverse force FyRe is obtained in an analogous manner, but with different coefficients in this for each proportional processing operation, these coefficients being in particular conditioned by the values of the wheel bases.
The combination of the signals generated by the proportional and integral, and proportional, respectively, processing operations applied to the first discrepancy and to the second discrepancy can be a linear combination, as in the example of
Thus, the regulator B2 modifies its outputs FyFe and FyRe on the basis of the discrepancies it receives as input, so as to reduce these discrepancies, which makes it possible to let the estimated values tend towards the actual values of the transverse forces.
In general, different regulators B2 can be implemented, for example, in the form of regulators of the proportional-integral-derivative type, or in the form of non-linear regulators.
The passage to discrete time leads to the following recurrent equations:
where T designates the time interval selected for the passage to discrete time, and is less than or equal to 1/1000th of second.
These equations are initialized with Vψe(0) at Vψ(0), γTe(0) at γT(0), and Vye(0) at 0. The values Vψ,(k−1) and γT(k−1) are the values of the yaw rate and of the transverse acceleration, respectively, measured at the instant t(k−1), i.e., at the instant t=T. (k−1).
The application of the method in a discrete time can thus be implemented in a processing unit including, for example, a microcontroller or a microprocessor adapted to perform, in real time, the algebraic operations that make it possible to determine the terms of the equations [8] and [9].
For the implementation discretized in real time, it is possible to introduce additional variables: εiγ which is the integral of the estimation error on the transverse acceleration, and εVψwhich is the estimation error on the yaw rate.
The variables are initialized with FyFe(0)=0, FyFe(0)=0, FyRe(0)=0, εiγe(0)=0 and Vψe(0)=Vψ(0).
At each instant t(k), i.e., T.k, the measurement values are recovered, with γT(k)=)γT(kT), and Vψ(k)=γψ(kT). Estimated values of these measurements, noted γTe(k) and Vψe(k), are then calculated from the transverse forces determined at the preceding instant t(k−1), with the following relationships:
These relationships result from the system of equations [5], the expression of Vψe(k) being obtained by integration of the second line of the system of equations [5]. The additional variables, noted εiγ and εVψ, are calculated according to the following relationships:
εiγ(k)=εiγ(k−1)+T(γT(k)−γTe(k)) and εV
The transverse forces for the instant t(k) are then determined according to the following relationships:
The process is then reiterated at the following instant t(k+1).
The magnitudes
constitute a front intermediary force and a rear intermediary force, respectively, these values being actualized at each iteration.
Taking into account the equations [11], the actualization of a current value of front intermediary force
consists simply in adding a value proportional to the first discrepancy, i.e.,
to obtain a new value of front intermediary force. The actualization of a current value of rear intermediary force is performed in a similar manner.
The determination of the estimated front and rear forces then simply consists in correcting the values of front and rear intermediary forces, by addition and by subtraction, respectively, of a corrective value which is proportional to the second discrepancy, this corrective value being
Thus, the invention offers a very simple method of evaluating the front transverse force and the rear transverse force which is based only on a measurement of transverse acceleration and a measurement of yaw rate.
The transverse acceleration and the yaw rate are, for example, coming from a dedicated measuring device including two accelerometers spaced apart from each other longitudinally with respect to the vehicle, these sensors making it possible to know the transverse acceleration to which the vehicle is subjected, and which results from the average of the values stemming from the two accelerometers.
The yaw rate results from the integration of the moment generated by the accelerations collected at these two accelerometers, about a vertical axis.
Thus, this method makes it possible to estimate the front and rear transverse forces without the need to use any elaborated specific model. In particular, it is not necessary to model the tires of the vehicle to evaluate the transverse forces.
Indeed, the standard bicycle model uses a model of tires which is linear. The standard bicycle model is then valid only up to a maximal transverse acceleration of 4 m/s2.
The method according to the invention does not use any tire model but it does not require a linear behavior of the tire either, so that the range of validity is not limited to transverse acceleration up to 4 m/s2.
The method according to the invention makes it possible to perform the evaluation of the front and rear force without the need to derive signals, but, on the contrary, by performing only integration operations. This method makes it thus possible to avoid the high risks that the implementation of signal derivation operations would induce.
An estimation of the transverse forces for each wheel can be determined from an estimation of the vertical loads of each wheel, resulting from a measurement or another. Indeed, the transverse force applied by the ground to a wheel is proportional to its vertical load. The transverse forces for each wheel can thus be determined from the equalities below:
in which:
FzLF: vertical load Left Front wheel
FzRF: vertical load Right Front wheel
FzLR: vertical load Left Rear wheel
FzRR: vertical load Right Rear wheel
FyLF: transverse force Left Front wheel
FyRF: transverse force Right Front wheel
FyLR: transverse force Left Rear wheel
FyRR: transverse force Right Rear wheel
Just like the measurement of the transverse forces, it is not possible to measure the vertical forces in real time in a direct manner at a cost compatible with mass production.
To remedy this drawback, the present invention proposes two estimation methods to estimate the vertical forces: a first, open-loop method, called static method, which is valid for constant longitudinal and transverse accelerations, and a second, closed-loop estimation, called dynamic estimation, which takes into account the dynamic properties of the vehicle.
Before describing these two methods, the various variables and parameters representative of physical magnitudes that will be used in reference to
The following physical magnitudes will thus be noted by:
Vx, Vy and Vz, the longitudinal, transverse, and vertical velocities, respectively;
Vθ, Vφ, and Vψ, the roll, pitch, and yaw rates, respectively;
FxLF, FxRF, FxLR, and FxRR, the longitudinal forces applied by the ground to the left front, right front, left rear, and right rear pneumatic tires, respectively;
FyLF, FyRP, FyLR, and FyRR, the transverse forces applied by the ground to the left front, right front, left rear, and right rear pneumatic tires, respectively;
FzLF, FzRF, FzLR, and FzRR, the vertical forces (load at the wheel) applied by the ground to the left front, right front, left rear, and right rear pneumatic tires, respectively;
ZaLF, ZaRF, ZaLR, and ZaRR, the displacements of the left front, right front, left rear, and right rear wheels, respectively, with respect to the body (distance between the wheel center and the upper attachment point of the suspension to the body);
a and b, the front and rear wheel bases, respectively,
E=a+b is the total wheel base,
v is half the distance between left and right wheels of the vehicle, and
h: height of the center of gravity G
The following will also be noted:
m: mass of the vehicle,
Iθ, Iφ, and Iψ, the rolling, pitching, and yawing moments, respectively,
g: the acceleration of gravity,
γx and γT: the longitudinal and transverse accelerations, respectively, of the vehicle, considered at the center of gravity G.
In the following, these same notations will be used to designate the signals representative of these magnitudes, respectively; signals stemming from measuring devices such as sensors or estimators.
To implement these methods, the vehicle is equipped with a device for estimating the load forces adapted to supply signals representative of the load force to which each wheel FzLF, FzRF, FzLR, and FzRR is subjected.
As illustrated on
In this first method, the vehicle is equipped with a measuring device supplying a signal representative of the measured longitudinal acceleration γx and this signal γx and the transverse acceleration γT, already available, are applied to the input of an estimator to supply estimated signals representative of the load force FzLFe, FzRFe, FzLRe, FRRe, respectively, to which each wheel is subjected.
The estimated vertical forces FzLFe, FzRFe, FLRe, FzRRe are then calculated from the following equations:
The second, so-called dynamic, estimation method, is illustrated by the block diagram of
The dynamic estimation in closed loop uses the same methodology as for the previously described estimation of the transverse forces.
This methodology is thus applied again, and it will thus not be described.
For this second method, the estimating device comprises a mechanical model of the vehicle, conform to that described on
This processing unit receives and processes the various measurements from the various above-mentioned measuring devices while being adapted to implement the various above-mentioned estimation methods.
The number and the choice of the measuring devices coupled to the processing unit depend on the method used.
Thus, for the method applying the bicycle model, two measuring devices are used: a device for measuring the yaw rate Vψand a device for measuring the transverse acceleration γT.
For the so-called static method applying the dynamic mechanical model of the vehicle, another measuring device is used in addition to the two previous ones: a device for measuring the longitudinal acceleration γx.
For the so-called dynamic method applying the dynamic mechanical model of the vehicle, eight other measuring devices are used: devices for measuring the displacements of the four wheels ZaLF, ZaRF, ZaLR, and ZaRR, respectively, a device for measuring the longitudinal velocity Vx, a device for measuring the vertical velocity Vz, a device for measuring the roll rate Vθ, and a device for measuring the pitch rate Vφ.
The velocity and acceleration measuring devices can be grouped together within a same inertial unit, disposed at the center of gravity G of the vehicle, and coupled to a navigation system of the GPS (Global Positioning System) type.
Number | Date | Country | Kind |
---|---|---|---|
0553787 | Dec 2005 | FR | national |