# Integrated Control of Hydromechanical Variable Transmissions

Authors: Shujun Yang; Yong Bao; Xianzhi Tang; Xiaojuan Jiao; Deqing Yang; Qing Wang
Journal: Mathematical Problems in Engineering
 (2015)

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## Abstract

A hydromechanical variable transmission (HMT) has advantages of continuous variation and high efficiency. So it is one of the ideal transmissions of heavy vehicles. The continuous speed varying process involves speed governing in range and range shift. Integrated control strategy of the HMT is proposed in this paper. The algorithm of the asymmetric saturated incremental proportional integral derivative (PID) speed control strategy in range and range shift conditions are derived. And this paper presents the range shift logic and range shift control strategies. A controller model is built in Matlab Simulink and cosimulated with the model of vehicle equipped with a two-range HMT. The HMT prototype hardware-in-the-loop simulation (HILS) platform of the integrated control strategy is built. The HILS results show that the range shift process is smooth and speed fluctuation does not happen. In the throttle stable stage, the engine speed is adjusted to the near optimal speed, and its change rules are in accordance with simulation results. The integrated control strategy is reasonable.


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## Body

## 1. Introduction

With the development of automotive industry, customers enhance the requirements of comfort and fuel-efficiency. Transmissions are important to satisfy the requirements [1, 2].The fundamentals and speed ratio characteristics of HMT are shown in Figure1. Input power is divided into two parts: hydraulic power and mechanical power in the power-split unit S. The hydraulic transmission H involves a variable displacement hydraulic pump and a fixed displacement motor. By changing the displacement of pump, the motor speed is controlled to vary continuously between the minimum (negative) and maximum (positive) speed, which is defined as a stroke. Each stroke is matched up with a working mode of the mechanical transmission M, which is defined as a range. Finally, two power flows converge into a continuously variable power flow in the conflux unit C.Figure 1
Fundamentals and speed ratio characteristics of HMT.
(a)
Fundamentals of HMT
(b)
Speed ratio characteristicsHMT is a new continuously variable transmission. It makes engine work in high efficient area, so it has the advantage of high efficiency. And it could transmit larger load than the belt type of continuously variable transmission (CVT). Hence, HMT is one of ideal transmissions for heavy trucks [3]. And it has been successfully applied to heavy vehicles [4–6].Based on lots of research effort on design and simulation of HMT, a series of methods for design and analysis have been established. Linares et al. [5] explained the basics of all types of CVT transmission and described the design parameters and fundamentals of a power-split system. Macor and Rossetti [7] optimized the design of a HMT and got a good speed convergence and a high average efficiency. To develop the control system of a HMT, Zhang and Zhuo [8] built a model of HMT using the principle of dynamics. Choi et al. [9] conducted a simulator for a tractor with HMT, under working and driving modes. And the tractor speed and the engine speed could be maintained at the desired values. Compared with the technologies of HMT design and analysis, control of HMT is still at an early developing stage.The speed varying process consists of speed governing in range and range shift. Therefore, the speed governing in range, timing of range shift, and methods of shift are all necessary. Lots of studies were about speed governing in range and control components. Yuan et al. [10] and Wei et al. [11] designed a variable parameter PID controller and studied a speed control system on HMT. In their researches, target speed ratio follow-up could be realized. But their researches focused only on speed ratio control in range. Hu et al. [12] explored the feasibility of shift without power interruption. Zhang and Zhuo [13] presented a speed variation and range shift method to achieve the widest speed range and avoid repeating shift. Savaresi et al. [14] designed a control system, including a servocontroller on valve, a servocontroller on hydraulic speed ratio, and a synchronizer. But improvements in tractor’s performance were obtained only by replacing the current pump/motor and speed detectors. Tanelli et al. [15] designed a control system for a tractor equipped with HMT, involving the control of one clutch and two clutch range shifts, and improved shift quality. An integrated control method of HMT is presented in the paper. A controller model is built in Matlab Simulink and cosimulated with the model of vehicle equipped with HMT. The HILS test of HMT is carried out.


## 2. The Integrated Control Strategy of HMT

A two-range HMT is shown in Figure2 and cited to illustrate the control method. The two-range HMT includes three planetary gear sets (K1,K2, and K3), two brakes (CH,CHM), one variable displacement pump (P), and one fixed displacement motor (M). In Figure 2, ni is the input speed of the HMT, and no is output speed of the HMT. When the brake CH is engaged and the brake CHM is released, the planetary gear set K1 works and the HMT works in hydraulic range (H). When the brake CHM is engaged and the brake CH is released, the planetary gear sets K2 and K3 work, and the HMT works in hydromechanical range (HM).Figure 2
A two-range HMT.The speed characteristics of HMT are made up of several associated infinitely variable ranges. Therefore, the integrated control strategy should involve speed control in range, range shift logic, range shift conditions, and shift control strategies.HMT speed is governed on the basis of vehicle speed and throttle opening. HMT makes engine and vehicle work in various ways in accordance with the selected mode, to achieve the expected performance.


## 3. Speed Control Strategy in Range

Speed control strategy in range changes the control current of hydraulic pump in accordance with the difference between the engine speed and ideal speed. Speed control strategy in range has been studied for many years, mainly in PID control and the speed ratio tracking control, and so forth [10–13].In certain road conditions, acceleration of the vehicle with HMT is limited by the engine torque and the maximum motor torque. The maximum motor torque is determined by the maximum pressure on the condition that the motor is selected.When the error between engine actual speednek and target speed nek∗ is greater during vehicle acceleration, the gradient of control current variety of the variable displacement pump ΔIp(k) increases according to PID algorithm. And the gradient of rotational speed variety of motor and vehicle acceleration resistance increase, which make hydraulic unit lose its ability to accelerate the vehicle after the pressure rises up to the maximum pressure. Therefore, when the vehicle accelerates, the upper saturation limit of ΔIp(k) must be set. When the vehicle decelerates rapidly, the speed ratio of HMT must be able to decrease quickly. So the lower saturation limit of ΔIp(k) in vehicle deceleration must be greater than that in vehicle acceleration. That is to say, the saturation limits of ΔIp(k) are asymmetric. In this paper, the asymmetric saturation incremental PID speed control strategy of HMT in range is proposed, and general algorithms in each range are derived.


### 3.1. Universal Incremental PID Algorithm

HMT controller refers to a digital PID control unit, and its increment is(1)Δuk=k0ek+k1ek-1+k2ek-2,where Δuk means the increment at t=kT and ei means the error at t=kTi(i=k-2,k-1,k); k0, k1, and k2 are coefficients, respectively, where k0=kp+kI+kD, k1=-(kp+2kD), k2=kD; kp refers to a scale factor, and kI refers to an integral factor, kI=kp(T/TI); kD refers to a derivative factor, kD=kp(TD/T); TD means the derivative time constant, TI means the integral time constant, and T means the sampling period.The output is(2)uk=uk-1+Δuk=uk-1+k0ek+k1ek-1+k2ek-2,where uk-1 is the sum of Δui(i=0~k-1).


### 3.2. The Asymmetric Saturation Incremental PID Speed Control Strategy in Range

The errorek of HMT controller is(3)ek=nek-nek∗,where nek and nek∗ are the engine speed and the ideal speed at t=kT, respectively.Equation (2) could be expressed as follows, if uk and Δuk are substituted by the pump current Ipk and the increment ΔIpk:(4)Ipk=IpmaxIpk-1±ΔIpk>IpmaxIpk-1±ΔIpkIpmin≤Ipk-1±ΔIpk≤IpmaxIpmin0≤Ipk-1±ΔIpk<Ipmin-Ipmin-Ipmin≤Ipk-1±ΔIpk<0Ipk-1±ΔIpk-Ipmax≤Ipk-1±ΔIpk<-Ipmin-IpmaxIpk-1±ΔIpk<-Ipmax(5)ΔIpk=ΔIpmaxk0ek+k1ek-1+k2ek-2>ΔIpmaxk0ek+k1ek-1+k2ek-2ΔIpmin≤k0ek+k1ek-1+k2ek-2≤ΔIpmaxΔIpmink0ek+k1ek-1+k2ek-2<ΔIpmin,where “±” is determined by HMT operating ranges. In direct proportion ranges, if gear ratio i≥0, plus sign is taken; if not, minus sign is taken. In inverse proportion ranges, if gear ratio i≥0, minus sign is taken; if not, plus sign is taken. In the two-range HMT, H range is a direct proportion range. In its positive half range, i≥0, the first “±” in (4) takes plus sign. And in the negative half range, i<0, the second one takes minus sign. The HM range is an inverse proportion range. Similarly, the first “±” in (4) takes minus sign, and the second one takes plus sign. Ip(k-1) refers to the pump current at t=(k-1)T. Ipmax and Ipmin are the upper and lower limits of the pump current. In the two-range HMT, the variable displacement hydraulic pump is a Sauer Danfoss Series 90 axial piston pump, where Ipmax=650±140mA and Ipmin=112±40 mA (Ipmin is designed for eliminating zero dead zone of the displacement control mechanism). ΔIpmax and ΔIpmin are the asymmetric saturated upper and lower limits of control current gradient, which depend on the displacement of pump/motor, speed ratio, vehicle resistance, and so forth.In Figure2, HMT output speed is a function of motor speed. And suitable PID parameters k0, k1, and k2 in (5) for each range must be selected by a large number of simulations and experiments to reduce the speed fluctuation of motor. Through theoretical calculations and simulations, parameters of the PID controller are as follows: k0H=0.008, k1H=-0.009, k2H=0.004 in H range, k0HM=0.010, k1HM=-0.009, k2HM=0.004 in HM range, ΔIpmax=2.4 mA, and ΔIpmin=-16 mA.


## 3.1. Universal Incremental PID Algorithm

HMT controller refers to a digital PID control unit, and its increment is(1)Δuk=k0ek+k1ek-1+k2ek-2,where Δuk means the increment at t=kT and ei means the error at t=kTi(i=k-2,k-1,k); k0, k1, and k2 are coefficients, respectively, where k0=kp+kI+kD, k1=-(kp+2kD), k2=kD; kp refers to a scale factor, and kI refers to an integral factor, kI=kp(T/TI); kD refers to a derivative factor, kD=kp(TD/T); TD means the derivative time constant, TI means the integral time constant, and T means the sampling period.The output is(2)uk=uk-1+Δuk=uk-1+k0ek+k1ek-1+k2ek-2,where uk-1 is the sum of Δui(i=0~k-1).


## 3.2. The Asymmetric Saturation Incremental PID Speed Control Strategy in Range

The errorek of HMT controller is(3)ek=nek-nek∗,where nek and nek∗ are the engine speed and the ideal speed at t=kT, respectively.Equation (2) could be expressed as follows, if uk and Δuk are substituted by the pump current Ipk and the increment ΔIpk:(4)Ipk=IpmaxIpk-1±ΔIpk>IpmaxIpk-1±ΔIpkIpmin≤Ipk-1±ΔIpk≤IpmaxIpmin0≤Ipk-1±ΔIpk<Ipmin-Ipmin-Ipmin≤Ipk-1±ΔIpk<0Ipk-1±ΔIpk-Ipmax≤Ipk-1±ΔIpk<-Ipmin-IpmaxIpk-1±ΔIpk<-Ipmax(5)ΔIpk=ΔIpmaxk0ek+k1ek-1+k2ek-2>ΔIpmaxk0ek+k1ek-1+k2ek-2ΔIpmin≤k0ek+k1ek-1+k2ek-2≤ΔIpmaxΔIpmink0ek+k1ek-1+k2ek-2<ΔIpmin,where “±” is determined by HMT operating ranges. In direct proportion ranges, if gear ratio i≥0, plus sign is taken; if not, minus sign is taken. In inverse proportion ranges, if gear ratio i≥0, minus sign is taken; if not, plus sign is taken. In the two-range HMT, H range is a direct proportion range. In its positive half range, i≥0, the first “±” in (4) takes plus sign. And in the negative half range, i<0, the second one takes minus sign. The HM range is an inverse proportion range. Similarly, the first “±” in (4) takes minus sign, and the second one takes plus sign. Ip(k-1) refers to the pump current at t=(k-1)T. Ipmax and Ipmin are the upper and lower limits of the pump current. In the two-range HMT, the variable displacement hydraulic pump is a Sauer Danfoss Series 90 axial piston pump, where Ipmax=650±140mA and Ipmin=112±40 mA (Ipmin is designed for eliminating zero dead zone of the displacement control mechanism). ΔIpmax and ΔIpmin are the asymmetric saturated upper and lower limits of control current gradient, which depend on the displacement of pump/motor, speed ratio, vehicle resistance, and so forth.In Figure2, HMT output speed is a function of motor speed. And suitable PID parameters k0, k1, and k2 in (5) for each range must be selected by a large number of simulations and experiments to reduce the speed fluctuation of motor. Through theoretical calculations and simulations, parameters of the PID controller are as follows: k0H=0.008, k1H=-0.009, k2H=0.004 in H range, k0HM=0.010, k1HM=-0.009, k2HM=0.004 in HM range, ΔIpmax=2.4 mA, and ΔIpmin=-16 mA.


## 4. Range Shift Logic

Range shift logic is the order of ranges. To realize continuously variable transmission, the HMT range switching elements such as the brakes must be sequentially controlled, and HMT can work in sequential range. The range shift logic of the two-range HMT is shown in Table1.Table 1
The range shift logic.
Range
Brake
C
H
C
HM
H range
Engagement
Disengagement
HM range
Disengagement
Engagement


## 5. Range Shift Conditions

The range shift refers to a transition process between two adjoining ranges. To improve shift quality, the shift conditions are as follows:(1)
The eventual output speed of HMT in current range should equal that of target range original point. In each range, closed-loop control is applied to control the motor speed. The ideal shift time is obtained in accordance with engine speed and motor speed.The target motor speednm∗ occurs at the ideal shift point where the speeds of driving and driven discs of the target brake are equal. In the two-range HMT, the ideal speed nm∗ from H range to HM range is derived:(6)nm∗=z0z2z1z5k2+1k1+1k1+k2+1k3+1ni,wherez0, z1, z2, and z5 are tooth numbers of gears from input shaft to K3, respectively; k1, k2, and k3 are the characteristic parameters of three planetary gear sets.(2)
The engine speed deviation (absolute value) must be greater than the minimum setting value. In order to avoid repeating shift, the minimum engine speed deviation must be set. Only when the engine speed deviation is greater than it would the range shift be allowed.(3)
The condition of the driver’s upshift must be satisfied. According to the traffic environment, the driver chooses a higher range through the range selector to limit vehicle speed. Only when the upshift is allowed by the range selector would the shift to a higher range be performed.To sum up, the conditions of upshift from H range to HM range are(7)nm≥nm∗ne-ne∗≥ΔnesetS=2.The conditions of downshift from HM range toH range are(8)nm≤nm∗ne-ne∗≤-Δneset,where S is the set value of the range selector. If S=0, HMT output speed is 0; if S=1, HMT can only run in H range; and when S=2, HMT can run in HM range. Δneset is the minimum engine speed deviation.


## 6. Range Shift Strategies

In range shift process, the brake of current range is released, and the brake of target range is engaged. Brake switching sequence is determined by range shift logic, and range shift start timets is determined by range shift conditions.The motor rotational direction is constant during range shift. But the change of motor torque direction leads to the exchange of the high and low pressure circuits. Meanwhile, the power flow of hydraulic system reverses. The motor speed is fluctuated by the sudden change in pressure and volumetric efficiency of hydraulic unit. At the same time, the speed characteristics of HMT vary sharply, and the power characteristics change, which lead to noise and vibration.It is range shift strategies that are responsible for the perfect engagement and disengagement of brakes to lower shift time and shock and to minimize input and output speed fluctuations [10]. Range shift strategies refer to control parameters and their control signals including variation, start time, and stop time. Range shift strategies in this work include the following:(1)
The overlap time between two brakes.Δtsi refers to the start time of oncoming brake to engage, and Δtss refers to the start time of offgoing brake to release. The overlap time between brakes is(9)Δts=Δtsi-Δtss.(2)
Oil buffer during the offgoing brake release. It is affected by start timeΔtsb1, end time Δtsb2, maximum pulse width γsmax, and pulse width change of proportional relief valve signal.(3)
Displacement adjustment of the pump. It is determined by start timeΔtsip1, end time Δtsip2, and displacement current variation ΔIs.The above start time and end time are time increments relative to range shift start timets.The timing and variation of the control variables of range shift strategies need to be determined by a number of simulations and experiments and are related to the following factors:(1)
The mechanical transmission scheme. Because of teeth matching in design of the mechanical transmission, the actual speed ratio of each range can not be equal to the ideal ratio of HMT, which is closely related to the displacement current variationΔIs.(2)
Response characteristics and volumetric efficiency of the closed hydraulic circuit. The displacement current variation can only be accomplished in range shift and may cause an impact if its timing is incorrect. That is, the displacement current may vary after the offgoing brake is disengaged. Its start timeΔtsip1 is greater than zero, and the end time Δtsip2 is related to response characteristics of the closed hydraulic circuit. The displacement current variation ΔIs is affected by volumetric efficiency of the closed hydraulic circuit.(3)
Parameters of the brake. The overlap timeΔts is affected by the hydraulic cylinder diameter and stroke of the offgoing and oncoming brakes. Pulse width change process and the maximum pulse width γsmax of the proportional relief valve are influenced by the torque coefficient of the friction plate, stiffness, and initial displacement of the return spring in the offgoing brake. Diameter and length of the hydraulic circuit for controlling brake also have an effect on control signals.Though the range shift strategies are different for different HMT schemes, there are several universal rules as follows:(1)
In upshift process from H range to HM range, the displacement current variationΔIs is negative, while in downshift process from HM range to H range, ΔIs is positive.(2)
Δtsi, Δtsip1, and Δtss are determined by lag time trr of control mechanism for variable displacement hydraulic pump and oil-filled time tcc of the brake. If trr≈tcc, then Δtsi=Δtsip1=0. If trr>tcc, then Δtsip1=0 and Δtsi=trr-tcc. If trr<tcc, then Δtsi=0 and Δtsip1=tcc-trr; Δtss is slightly less than tcc.(3)
The minimum oil pressurepγsmin of the oil pressure buffering needs to be greater than the minimum oil pressure to move piston of the brake.According to the simulation results, the range shift strategies fromH range to HM range are as follows: Δtsi=Δtsip1=Δtsb1=0, Δtss=Δtsip2=Δts=0.1s, and Δtsb2=0.2s; ΔIs=-14 mA; γsmax=0.10, as shown in Figure 3. The control signals from HM range to H range are the same as upshift in value and time, except for ΔIs=14 mA.Figure 3
The range shift strategies from H range to HM range.


## 7. Simulation of Control Strategies

According to the control strategies, the model of controller is built in Matlab Simulink (Figure4) and cosimulated with the model of a vehicle equipped with the two-range HMT. The vehicle model is built in MSC Easy5 [16]. The results are shown in Figure 5.Figure 4
The controller model built in Matlab Simulink of the two-range HMT.Figure 5
Dynamic response of vehicle.
(a)
(b)
(c)
(d)When the coefficient of rolling resistance equals 0.02, the throttle opening is shown in Figure5(a). Control signals and speeds are shown in Figures 5(b), 5(c), and 5(d).Before engine throttle is open (beforet=5s), the brake CH is engaged, and the other is disengaged. Engine is in idle state, HMT is in neutral range, and vehicle is parked. With the throttle opening (t=5s), control signal IP begins to increase, HMT changes to H range, and the vehicle launches.At the time oft=11.2s, the HMT range shift conditions are satisfied from H range to HM range, and the controller begins to run range shift strategies (shown in Figure 3). During the range shift (t=11.2s–11.6s), the signal of brake CH decreases, and the signal of brake CHM increases gradually. The displacement current decreases by 14 mA (ΔIs=-14mA), and the rotational speed of engine fluctuates slightly. After the range shift, HMT comes into HM range. With the displacement of hydraulic pump decreasing, the vehicle accelerates in the HM negative half range. At the time of t=21s, HMT passes the zero point into the HM positive half range, at which displacement is zero. In the HM positive half range, with displacement of hydraulic pump increasing reversely, the vehicle accelerates.With the throttle decreasing and the target engine speed decreasing, the displacement current increases reversely until the actual engine speed is lower than its target speed. At the time oft=27.5s, the vehicle speed starts to come down. At the time of t=35s, engine throttle closes, the target engine speed steps, and the displacement current changes a lot. At the time of t=40.5s, HMT falls back to the HM positive half range, and vehicle decelerates continuously. At the time of t=44.2s, HMT comes into range shift from HM to H range, the control signal of brake CHM decreases gradually with the control signal of brake CH increasing. The displacement current increases by 14 mA (ΔIs=14mA), the engine speed also fluctuates slightly, and HMT changes into H range. At the time of t=46s, HMT turns back to neutral range.In Figure5, the control current of hydraulic pump does not fluctuate in range. There is no repeating shift. Engine drops to the idle speed after HMT turns back to neutral range.The ideal and actual speeds of engine are shown in Figure5(c). The launch of vehicle takes 1.2 s (from 5 s to 6.2 s). After vehicle launches, ne is obviously larger than ne∗. From t=6.2 s, as the engine load is heavier, ne drops fast to a little higher than ne∗. After that, ne keeps close to ne∗, and the maximum difference is 44 r/min (except for the zero points of hydraulic pump and range shifts). ne drops to less than ne∗, after the throttle closes. ne quickly declines down to ne∗. Because of the vehicle inertia, the actual engine speed remains for some time (about 10.1 s), with the adjustment of HMT. When the vehicle speed approximately equals zero, the engine drops fast to idle speed.The vehicle speedua is shown in Figure 5(d). With vehicle launching, accelerating, decelerating, and stopping, speed fluctuation does not happen, during range shifts or at the zero points.


## 8. Hardware in the Loop Simulation

The HILS of HMT is a test method, on the basis of the computer simulation system. In the HILS test, the HMT object replaces the HMT model in the simulation circuit. And it is directly controlled by the controller through input/output devices and interface circuit.Due to the HMT object connected to the simulation circuit, this test can further prove the reliability of simulation results. This method can check the correctness of control strategy on the basis of HMT computer simulation and adjust control parameters accurately. It can also check the correctness of HMT simulation model. It is especially effective for using a gray box model to describe the HMT which is difficult to describe by a mathematical model.Based on 330 kW dynamic simulation test bench, the original load objects drive and load the HMT according to the engine and vehicle dynamic characteristics through the real-time model driving. In this system, the HMT is a material object, and the other parts are all models or are driven by models. The HILS system is shown in Figure6. And some objects of the HILS test are shown in Figure 7.Figure 6
The HILS system of HMT.Figure 7
Some objects of the HILS test.
(a)
(b)The HILS software of HMT is made up of the HMT controller model, the engine model, vehicle real-time models, and real-time windows target. Under the control of the engine real-time model, load component 2 of the dynamic simulation test bench which runs according to the engine characteristics provides power for the HMT. Under the control of the vehicle real-time model, load component 1 loads the HMT according to the vehicle traffic characteristics. The controller model does real-time control of HMT according to the control strategies. The HMT adjusts speed ratio according to the change of vehicle working conditions, which makes the engine run at the approximately optimal speed (the best fuel economy or the best performance).The input of engine real-time model is the load torqueTq, and the output is the engine speed ne. On the dynamic simulation test bench, the load component 2 simulating engine is under the control of constant speed mode. Speed and torque detector 2 feeds load torque back to a simulation computer. The calculation result of the engine real-time model is given to load component 2.The engine real-time model can be described as(10)Jeω˙e=Teα,ne-TqSoω˙e=Teα,ne-TqJene=602π∫ω˙eVe=neAω,where Je is the simulated engine’s inertia, Te(α,ne) is the static output torque of simulated engine, Tq is the load torque by feedback of speed torque sensor, ne is the output speed of the load component 2, Ve is the control voltage of the load component 2 controller, and Aw is the control voltage linear conversion coefficient of the load component 2.In the computer simulation model, the input and output of vehicle model are the output speed and load torque of HMT, respectively. On the dynamic simulation test bench, load component 1 simulating vehicle is under the control of constant torque mode. To ensure that input and output are consistent with calculation in the simulation model, “virtual axis” needs to be introduced to the vehicle real-time model.The output torque of the vehicle real-time model is(11)Td1=∫kω-ω1dt+cω-ω1ω˙1=Td1-Ff+FW+Fi+Fbr/i0mr2/i02-Jd1VT=Td1AT,where k is the torsional stiffness of virtual axis, c is the damping of virtual axis, Td1 is the output torque of the vehicle real-time model, ω is the feedback speed signal of the speed sensor, ω1 is the angular speed of vehicle equivalent inertia, VT is the control voltage of the load component 1 controller, and AT is the control voltage linear conversion coefficient of the load component 1.Under load component 1 working without load by manual control mode, the HMT range shift test results are shown in Figure8. The figures show that the range shift process is smooth and speed fluctuation does not happen. It demonstrates that the control strategy of range shift determined by the motor speed is reasonable. When the load increases, the output speed fluctuates clearly in range shift process. It states that the range shift control strategies are necessary.Figure 8
The test results of the HMT range shift process.
(a)
(b)
(c)
(d)When load components 1 and 2 are automatically controlled, the curve of the engine throttle is shown in Figure9(a), and the HMT responses are shown in Figure 9(b). The main performance indicators are shown in Figures 9(c) and 9(d). From Figure 9, with engine throttle changing, the HMT speed ratio changes under the control of the controller model. In the throttle stable stage, the engine speed is adjusted to the near optimal speed, and its change rules are in accordance with simulation results. Because of the adjustment of engine performance and vehicle inertia, the engine can work at its top speed for a long time.Figure 9
The vehicle dynamic characteristics.
(a)
(b)
(c)
(d)


## 9. Conclusions

(1)
The integrated control strategy of HMT is proposed. The algorithm of the asymmetric saturated incremental PID speed control strategy in range and range shift conditions are derived. And this paper presents the range shift logic and range shift control strategies.
(2)
A controller model is built in Matlab Simulink and cosimulated with the model of vehicle equipped with a two-range HMT. Simulation results indicate that under the control of the proposed strategies the engine runs near ideal speed, and the vehicle meets driving requirements with the throttle changing.
(3)
The HILS test of HMT is carried out. The test results show that the range shift process is smooth and speed fluctuation does not happen. In the throttle stable stage, the engine speed is adjusted to the near optimal speed, and its change rules are in accordance with simulation results.
(4)
The results demonstrate that the HMT model is correct, and the control strategy is reasonable. The system of HILS works reliably and meets the requirements of the HMT dynamic characteristics study.



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*Source: 290659-2015-09-07.xml*