 Original Article
 Open Access
 Published:
Modeling and Parameter Sensitivity Analysis of ValveControlled Helical Hydraulic Rotary Actuator System
Chinese Journal of Mechanical Engineering volume 35, Article number: 66 (2022)
Abstract
As a type of hydraulic rotary actuator, a helical hydraulic rotary actuator exhibits a large angle, high torque, and compact structure; hence, it has been widely used in various fields. However, its core technology is proprietary to several companies and thus has not been disclosed. Furthermore, the relevant reports are primarily limited to the component level. The dynamic characteristics of the output when a helical rotary actuator is applied to a closedloop system are investigated from the perspective of driving system design. Two main aspects are considered: one is to establish a reliable mathematical model and the other is to consider the effect of system parameter perturbation on the output. In this study, a detailed mechanical analysis of a helical rotary hydraulic cylinder is first performed, factors such as friction and load are considered, and an accurate dynamic model of the actuator is established. Subsequently, considering the nonlinear characteristics of pressure flow and the dynamic characteristics of the valve, a dynamic model of a valvecontrolled helical rotary actuator angle closedloop system is described based on sixthorder nonlinear state equations, which has never been reported previously. After deriving the system model, a sensitivity analysis of 23 main parameters in the model with a perturbation of 10% is performed under nine operating conditions. Finally, the system dynamics model and sensitivity analysis results are verified via a prototype experiment and cosimulation, which demonstrate the reliability of the theoretical results obtained in this study. The results provide an accurate mathematical model and analysis basis for the structural optimization or control compensation of similar systems.
Introduction
Helical hydraulic rotary actuators (HHRAs) are hydraulic actuators that convert hydraulic energy into mechanical energy via rotary motion [1]. Compared with conventional rotary hydraulic actuators, such as vane, rack, and gear type ones, helical rotary actuators offer a large rotation angle, high output torque, compact structure, and high volumetric efficiency owing to their unique double helical pair structure [2, 3]. The rotation angle range of a helical actuator can be designed to exceed 360°. Furthermore, for the same rotation angle range, the helical actuator typically exhibits a small weight and volume, which renders the structure installed with it compact [4]. Furthermore, the helical actuator can achieve a higher actuating pressure than the conventional rotary actuator. It can maintain a high efficiency at 21 MPa, which cannot be realized by other forms of hydraulic rotary actuators [5]. Because of these outstanding characteristics, helical rotary actuators have been widely used in certain applications that require large torques, large rotation angles, and limited installation space, e.g., agricultural, construction, and mining machinery [6, 7]. However, only a few companies can manufacture such actuators currently [6,7,8,9], and the core technologies for design and manufacturing remain proprietary. Studies regarding HHRAs, in addition to some patents [10,11,12], focus primarily on the component level, including the structural design, dynamic models, flow field analysis, transmission efficiency, and sealing [13,14,15,16].
The performance of a valvecontrolled actuator system, as a driving unit, directly affects the control performance of the entire machine [17]. Such systems are typically designed using mathematical models derived from constantcoefficient ordinary differential equations [18]. However, two problems are encountered: First, studies regarding helical rotary actuator driving systems are scarce. Furthermore, the dynamic model of the rotary actuator described in the literature is relatively simple [2, 3] and may not be sufficiently accurate when modeling analysis is required. Therefore, reliable mathematical models for the design and analysis of hydraulic systems are insufficient. The other problem is that the parameters in the model are typically regarded as constants [19]; however, these parameters may not be consistent with the parameters in practical applications because the system parameters are time varying [20]. For example, structural wear results in parameter changes, inaccurate valve test parameters, and pressure fluctuations in the hydraulic system. To obtain a valvecontrolled actuator system that satisfies the design requirements, the effect of parameter perturbation on the dynamic characteristics of the system is to be investigated; therefore, a sensitivity analysis of the system parameters is required.
Sensitivity analysis can be performed via several methods, which can be classified into sensitivity functions in the time domain, frequency domain, and the performanceindex sensitivity, each of which offers its own advantages and application range [21]. Sensitivity analysis theory is widely used in mechanical design, power systems, water conservancy systems, etc. [22,23,24]. In the application of hydraulic systems, trajectory sensitivity analysis in the time domain is most typically used method and can be used for nonlinear systems with timevarying parameters. Vilenius et al. [20] introduced and applied a sensitivity model suitable for deadbandtype nonlinearities in a typical servo system used in the sawmill industry. They simplified the valvecontrolled actuator system into a fifthorder model and derived a firstorder trajectory sensitivity mathematical expression of the system. Under a single operating condition, the sensitivity of the system parameters was defined when the 10 main parameters changed by 1%. Kim et al. [25] used a fourthorder state equation to analyze the nonlinear dynamics of an axial piston pump system and analyzed the sensitivity of the parameters in the model using a firstorder sensitivity equation. Pietola et al. [26, 27] investigated the transientstate and steadystate parameter sensitivity of a heavily loaded flexible electrohydraulic position servo system and then compared three control methods, i.e., Pcontrol, model reference control, and P + PID/\(\dot{{\rm x}} \)control. Farahat et al. [21] constructed a fourthorder linear mathematical model of an electrohydraulic servo position control system. The position control sensitivity of the valvecontrolled actuator system to 18 main parameters based on a 1% change is investigated, and four sensitivity indices are presented. Kong et al. [28, 29] established a sixthorder nonlinear model of a valvecontrolled actuator system based on position control, and the influence degree and rules of 10% parameter changes with respect to the displacement output response were obtained using the firstorder trajectory sensitivity method. Subsequently, they deduced the method of secondorder trajectory sensitivity and analyzed its effect on the system displacement step response with parameter variation (10% and 20%) under nine operating conditions. Ba et al. [30,31,32] proposed a firstorder sensitivity matrix method and applied it to the dynamic sensitivity analysis of the valvecontrolled actuator system of a legged robot. Huang et al. [33] used the firstorder trajectory sensitivity method to determine the dominant parameters of the electrohydraulic actuator in a legged robot and then estimated them online in real time.
The main difference among the studies above is the degree of simplification of the hydraulic system model. The sensitivity analysis methods are similar and are based on trajectory sensitivity. However, the hydraulic actuators reported in the literature are linear actuators, and a sensitivity analysis of the helical rotary actuatordriven system has not been reported. Compared with linear actuators, helical rotary actuators are more complex in terms of structure, and their model parameters are numerous; therefore, the results of parameter sensitivity analysis for those two types of actuators may be different.
To design and analyze the dynamic characteristics of a valvecontrolled helical rotary actuator system, in this study, a relatively accurate dynamic model of an actuator was established. A mechanical analysis of the designed helical rotary actuator was performed, and the friction between different components and load types was considered. Subsequently, considering the nonlinear characteristics of pressure and flow at the valve port and the dynamic characteristics of the servo valve, a sixthorder nonlinear state equation was established to describe an angular displacement closedloop hydraulic system. Under different step input and load conditions, the sensitivities of 23 parameters in the closedloop system model were solved using the firstorder trajectory sensitivity analysis method. Finally, the dynamic model and sensitivity analysis results of the system were verified by experiments and cosimulation, respectively, and a sensitivity index was used to explain the sensitivity results comprehensively.
The remainder of this paper is organized as follows: In Section 2, a dynamic model of the helical rotary actuator is deduced, and a mathematical model of the closedloop system is presented. The parameter sensitivity equation of the system is presented in Section 3. Details regarding the experiment and cosimulation verification are provided in Section 4. Finally, a summary is presented in Section 5.
Nonlinear Dynamic Model of System
The angular displacement closedloop system of a valvecontrolled HHRA is the research object of this study. In the following, the dynamic model of the rotary actuator is first established, and then the servo valve and proportional controller are introduced to establish the model of the entire hydraulic system.
Basic Operating Principle of HHRA
The basic structure of the designed HHRA is shown in Figure 1. It is primarily composed of a housing with an integral ring gear and two moving components: an output shaft and an annular piston sleeve. A_{1} and B_{1} represent the oil inlet and outlet, respectively. The helical spline teeth on the outside diameter of the piston engage in matching the splines of the housing ring gear (helical pair G_{1}), and the inside diameter of the piston houses a second set of splines of the opposite hand, which engages the matching splines of the output shaft (helical pair G_{2}). The seal ring on the piston segregates the housing into two independent chambers. When hydraulic pressure is applied, the piston actuates axially relative to the housing, similar to a hydraulic linear actuator. Simultaneously, owing to G_{1}, the piston rotates and finally exhibits helical motion. When the piston is actuating helically, it drives the output shaft to rotate under the action of G_{2}. Therefore, the rotational direction of the output shaft can be controlled by filling the pressure oil into different oil ports (A_{1} or B_{1}).
Dynamic Model of HHRA
Based on the operating principle described in the previous section, the HHRA is schematically illustrated (as shown in Figure 2). It is composed of a piston (label 1), an output shaft (label 2), housing (label 3), and bearings (labels b_{1} and b_{2}). The housing was fixed, and the axial displacement of the output shaft was limited by the bearings. The relative motion components are primarily G_{1} and G_{2}, i.e., the helical motion of the piston and the rotation of the output shaft, respectively. To facilitate analysis, it is assumed that the pressure oil is introduced into the left chamber of the actuator, and the right chamber of the actuator returns oil. The motion states of the piston and shaft in this case are shown in Figure 2.
Kinematic analysis should first be performed prior to dynamic modelling. Because the HHRA is a system with one degreeoffreedom, once the displacement or rotation angle of the piston is determined, the motion state of the entire system can be determined. The state variables exhibit the following kinematic relationships:
where \({\varphi }_{1}\) is the rotation angle of the piston relative to the housing; \({\varphi }_{2}^{1}\) is the angle of the output shaft relative to the piston; \({\varphi }_{2}\) is the angle of the output shaft relative to the housing; x_{a1} is the axial displacement of the piston; S_{1} and S_{2} are the leads of G_{1} and G_{2}, respectively. After obtaining the kinematic relationship, a mechanical analysis of the piston and output shaft was performed, an illustration of which is presented in Figure 3.
The forces and moments exerting on the piston are shown in Figure 3(a). Considering the coordinate system direction in the figure as the positive direction, the dynamic equations of the piston can be expressed as follows:
where F_{hyd} is the resultant force generated by the oil pressure in the two chambers of the actuator; m_{1} is the mass of the piston; J_{1} is the moment of inertia of the piston; F_{1,3} and F_{1,2} are the axial forces generated by G_{1} and G_{2} respectively; T_{1,3} and T_{1,2} are the torques generated by G_{1} and G_{2}, respectively; f_{1,3} and T_{f1,3} are the force and torque caused by friction between the seal ring on the piston and housing, respectively. The moments on the output shaft (as no movement exists in the axial direction of the output shaft, only the moments are presented herein) are shown in Figure 3(b). Considering the load characteristics, the dynamic equation is expressed as follows:
where T_{2,1} is the torque generated by G_{2}; T_{2,1} = T_{1,2}; T_{2,b1} and T_{2,b2} are the torques generated by the bearing friction; J_{2} is the moment of inertia of the output shaft and load; B_{l} is the load damping coefficient; K_{l} is the load stiffness coefficient; T_{l} is the external load torque. Meanwhile, forces F_{1,3}, F_{1,2} and torques T_{1,3}, T_{1,2} caused by G_{1} and G_{2} can be obtained via a mechanical analysis of the helical pair, as shown in Figure 4.
Because the effect of piston gravity on the helical pair depends on the installation position, to simplify the analysis, the output shaft is assumed to be installed horizontally; thus, the effect of gravity is negligible. As shown in Figures 4(a) and (b), F_{1,3}, T_{1,3}, F_{1,2}, and T_{1,2} are calculated as follows:
where N_{1,3} and N_{1,2} are the normal forces produced by G_{1} and G_{2}, respectively; μ_{1} and μ_{2} are the dynamic friction coefficients of G_{1} and G_{2}, respectively; Ψ_{1} and Ψ_{2} are the helix angles of G_{1} and G_{2}, respectively; d_{1} and d_{2} are the pitch diameters of G_{1} and G_{2}, respectively. The resultant force generated by the oil pressure F_{hyd} can be expressed as
where p_{1} is the oil pressure in the left chamber of the actuator, p_{2} the pressure in the right chamber, and A_{p} the effective action area of the piston. According to Eqs. (1)–(11), the dynamic equation of the HHRA can be expressed as follows:
where \(A = Q_{1} \cdot \left( {\frac{{J_{1} S_{2} }}{{S_{1} + S_{2} }} + J_{2} } \right) + Q_{2} \cdot J_{2} + \frac{{m_{1} S_{1} S_{2} }}{{2\pi \left( {S_{1} + S_{2} } \right)}}\),
\(B = \left( {Q_{1} + Q_{2} } \right) \cdot B_{l},\) \(C = \left( {Q_{1} + Q_{2} } \right) \cdot K_{l},\)
\(\begin{gathered} D = Q_{1} \cdot \left( {T_{f1,3} + T_{{2,\rm{b}1}} + T_{{2,\rm{b}2}} + T_{l} } \right) + \hfill \\ \, Q_{2} \cdot \left( {T_{{2,\rm{b}1}} + T_{{2,\rm{b}2}} + T_{l} } \right) + f_{1,3} , \hfill \\ \end{gathered}\)
\(Q_{1} = \frac{{2(\cos \lambda_{1} + \mu_{1} \sin \Psi_{1} )}}{{d_{1} (\sin \lambda_{1}  \mu_{1} \cos \Psi_{1} )}}\), \(Q_{2} = \frac{{2(\cos \lambda_{2} + \mu_{2} \sin \Psi_{2} )}}{{d_{1} (\sin \lambda_{2}  \mu_{2} \cos \Psi_{2} )}}.\)
Dynamic Model of ValveControlled HHRA System
In this study, an angle closedloop system is investigated using a servo valve, and a schematic diagram of the valvecontrolled actuator system is shown in Figure 5. The flow at the valve port is expressed as follows:
where x_{v} denotes the valve spool displacement, p_{s} the supply pressure, p_{0} the return oil pressure, and K_{d} the converted flow coefficient. Considering the effects of oil leakage and compressibility, the flow continuity equations for the HHRA can be written as follows:
where β_{e} is the effective bulk modulus of the system; V_{g1} and V_{g2} are the volumes of the oil inlet and outlet channels connecting the valve and actuator, respectively; L is the maximum axial stroke of the piston; L_{0} is the initial axial position of the piston; C_{ip} is the internal leakage coefficient of the actuator; C_{ep} is the external leakage coefficient.
A secondorder differential equation was used to approximate the dynamics of the servo valve, as follows:
where ζ is the damping ratio of the valve, ω the natural frequency of the valve, K_{axv} the gain of the valve, and I the input signal of the valve. The characteristics of the angle closedloop control can be expressed as follows:
where K_{p} is the gain of the P controller, and u is the input signal. The block diagram of the valvecontrolled HHRA system based on the angular displacement closedloop control is established using Eqs. (12)–(18), as shown in Figure 6.
The statespace equation is used to describe the sixthorder system, and the state variables are selected as follows:
The state equation of the valvecontrolled HHRA system is obtained as follows:
where \(\Gamma = \frac{{A_{p} S_{1} S_{2} }}{{2\pi (S_{1} + S_{2} )}}\),
\(\Delta_{1} = \frac{{[1 + {\text{sgn}} (x_{\rm{v}} )]p_{\rm{s}} }}{2} + \frac{{[  1 + {\text{sgn}} (x_{\rm{v}} )]p_{0} }}{2}  {\text{sgn}} (x_{\rm{v}} )p_{1}\),
\(\Delta_{2} = \frac{{[1  {\text{sgn}} (x_{\rm{v}} )]p_{\rm{s}} }}{2} + \frac{{[  1  {\text{sgn}} (x_{\rm{v}} )]p_{0} }}{2} + {\text{sgn}} (x_{\rm{v}} )p_{2}\), here, \({\varphi }_{20}\) is the initial angle of the output shaft, and \({\varphi }_{2\mathrm{max}}\) is the maximum angle of the output shaft.
Sensitivity Model and Analysis
The actual system parameters exhibit varying degrees of perturbation. When the system is sensitive to certain parameters, this perturbation will render the actual output significantly different from that of the mathematical model, which may result in deviation from the design requirements. Analyzing the parameter sensitivity allows us identify these key parameters such that the appropriate response measures can be implemented to reduce the parameter sensitivity or the parameters can be optimized. In this study, the firstorder sensitivity method was selected to analyze the effect of 10% perturbation from the nominal parameter value on the rotation angle of the output shaft \({\varphi }_{2}\). This method is sufficiently accurate and allows an easier calculation than the highorder sensitivity method [29].
FirstOrder Trajectory Sensitivity Equation of System
Based on Eq. (19), many different types of parameters exist in the system dynamics model, including the structural parameters of the HHRA, operating parameters, parameters of the servo valve, and control parameters. The fluctuations of the different parameters are of different timescales. In this study, 23 main parameters in the system model were selected, which encompassed all types of parameters, as follows:
The actual structural parameters of the HHRA (α_{1}–α_{13}) are associated with the manufacturing errors and wear degree of the corresponding parts. Therefore, they will not change in the short term but may change after the system operates for a long time owing to wear. Owing to changes in the gas content, oil temperature, and load conditions, the operating parameters (α_{14}–α_{19}) are not constant but in a state of rapid dynamic fluctuation. Because the nonlinear highorder dynamic characteristics of the servo valve are simplified into a secondorder differential equation, the real dynamic characteristics cannot be fully described. Therefore, the parameters of the servo valve (α_{20}–α_{22}) are not fixed and are affected by the input signal and operating parameters. The control parameter α_{23} must be dynamically adjusted with the change in system conditions to maintain the robustness of the system performance. Because the parameters above may exhibit different degrees of perturbation, the effects of the variations in the parameters above on the output characteristics of the system must be analyzed to improve the performance of the system.
The dynamics and sensitivity equations of the closedloop system can be expressed as follows [20]:
where \({{\varvec{\lambda}}}^{{\varvec{i}}}={\left(\frac{\partial {\varvec{x}}}{\partial {\alpha }_{i}}\right)}_{{\varvec{\rm{n}}}}\) is the sensitivity function of parameter α_{i}, i = 1,…,23.
The vector is written as follows:
Assuming that the initial state is zero, the initial conditions for Eq. (20) are
Once the sensitivity functions are obtained, the variation of the state caused by parameter perturbation can be determined using the following equation (based on the Taylor theorem and disregarding higherorder terms):
Solutions of Sensitivity Function
To solve Eq. (20), the values of the nominal parameters are determined, as shown in Table 1. The structural parameters of HHRA are consistent with those in the threedimensional (3D) model. The parameters of the servo valve were obtained from the dynamic characteristic curve in the stylebook. The values of the operating parameters, control parameters, and other parameters that are difficult to determine were selected based on application requirements and engineering experience.
Second, Eq. (20a) was established and solved using MATLAB SIMULINK to obtain the state x at every moment. The step input is generally believed to be the most severe operating state of the system; therefore, the step signal was used as the input signal to evaluate the dynamic performance of the system. The dynamic response characteristics of the system were different under different values of angular displacement and load conditions. Therefore, to encompass various operating conditions, step signals of 45°, 90°, and 135° were used as inputs, and the external load torques of “no load,” 100 N·m, and 200 N·m were used, respectively. The step response of the angular displacement closedloop system was solved under nine operating conditions, all of which are listed in Table 2.
After solving the state equations, the state value of each moment within the calculation duration was obtained. The results were converted into the coefficient matrix and free matrix of Eq. (20b). Subsequently, using MATLAB, the fourthorder Runge–Kutta method was applied to solve the firstorder trajectory sensitivity equations. Finally, the sensitivity functions of the angular displacement step response to 23 parameters were obtained under nine different conditions. Because the sensitivity function curves of some parameters are of different orders of magnitude under noload and load conditions, for brevity, only the sensitivity function solutions of different step signals under noload conditions are presented herein, as shown in Figure 7.
The curve in Figure 7 shows the dynamic sensitivity of each parameter to the rotation angle of the output shaft within 0.3 s. Owing to the different ranges of nominal values, the sensitivity functions of different parameters exhibit different orders of magnitude, rendering it difficult to intuitively compare the sensitivity of various parameters from the figure. Eq. (22) was used to clarify the results, and the variation in the angle was obtained based on the sensitivity function of different parameters to uniformly characterize the effect of each parameter. The effect of 10% fluctuation of each parameter on x_{1} under the nine conditions is illustrated in Figure 8.
As shown in Figure 8, under the noload conditions, the parameters that are the most sensitive to the rotation angle are α_{12}, α_{17}, α_{22}, and α_{23}, in which the curves corresponding to α_{17}, α_{22}, and α_{23} are exactly the same. This is followed by parameters α_{3}, α_{4}, α_{18}, α_{20}, and α_{21}, whereas the other parameters barely affect the rotation angle. However, as the load increases, parameters α_{5}, α_{6}, α_{9}, and α_{10} becomes more sensitive gradually, and their effect on the rotation angle is not negligible. Meanwhile, some parameters fluctuated during the initial stage. The amplitude of the fluctuation increases with the load but decays rapidly. Only qualitative results can be obtained, and a more detailed quantitative analysis of the sensitivity of each parameter is presented in Section 4.3.
Experiment and CoSimulation Verification
A valvecontrolled actuator test platform was constructed to verify the accuracy of the system dynamics model in this study. Subsequently, the theoretical calculation results of parameter sensitivity were verified via cosimulation. To validate the theoretical sensitivity results, the effect of slight parameter changes on the system must be analyzed. However, slight changes in some parameters are difficult to measure accurately in the prototype experiment. For example, pressure pulsation occurs in the system pressure, and the pressure sensor may be affected by noise; therefore, accurately increasing or decreasing the pressure by approximately 10% is challenging. Moreover, the structural parameters or some operating parameters cannot be changed in the prototype experiment. Hence, the results of the sensitivity analysis were verified via cosimulation using MATLAB and Adams.
Dynamic Model Verification of ValveControlled HHRA System
The valvecontrolled HHRA test platform and a schematic diagram of the system are shown in Figure 9. The closedloop system primarily includes a rotary actuator, a servo valve, a valve controller, an encoder, diaphragm coupling, a magnetic powder brake, and auxiliary connections. One end of the output shaft of the actuator is equipped with the encoder, and the other end is connected to the brake through coupling. The encoder feeds back the angle signal to the valve controller, which processes the desired signal and feedback signal, and then outputs the control signal to the servo valve. The brake is used for loading, and the load torque can be set using its proprietary controller.
The setting of the experimental parameters is consistent with the nominal values presented in Table 1, and step response experiments were performed under the nine operating conditions. The rotation angle signal fed back by the encoder was written into the computer via an acquisition card, and the acquisition frequency was 1000 Hz. After filtering the data, step curves were obtained under all operating conditions, as shown in Figure 10(a). The rise time was regarded as the evaluation index of the system dynamic performance (i.e., the time when the initial value reaches 90% of the steadystate value), and the experimental results were compared with the calculation results of the theoretical model, as shown in Figure 10(b). The comparison results show that under various operating conditions, the maximum error between the theoretical rise time and the experimental value did not exceed 7%, which verifies the accuracy of the system dynamics model established in this study.
Verification of Sensitivity Solution Results
As mentioned above, the sensitivity solution was verified via cosimulation. First, the cosimulation model was established using MATLAB and Adams, and then four parameters showing rapid changes in the time scale were selected for sensitivity verification.
CoSimulation Model
First, the 3D model was imported into Adams; subsequently, constraints and contacts were added. For the moving components, a revolute joint was added to the output shaft, and a cylindrical joint was added to the piston. For other components, such as the housing and bearings, fixed pairs were added. Contacts were added between the piston and output shaft, as well as between the piston and housing. Hertz contact theory was used to calculate the contact force, and the corresponding contact parameters are listed in Table 3.
The plant was controlled using Adams. The hydraulic thrust F_{hyd} was used as the input signal of the system, and the output signals were the rotation angle and angular velocity of the output shaft. Finally, by combining Eqs. (13)–(18) and the Adams control plant, the cosimulation model for the valvecontrolled HHRA system was established in MATLAB SIMULINK, as shown in Figure 11. Next, the parameter sensitivity problem was solved using the cosimulation model and compared with the theoretical calculation results to complete the verification.
Verification of Parameter Sensitivity
To obtain the sensitivity solution from the cosimulation model, a certain parameter was changed by 10% while other parameters were maintained at the nominal value; subsequently, simulations were conducted to obtain the step response curve of the output shaft. By calculating the difference between the obtained curve and the curve prior to the parameter changes, the effect of the parameter change on the dynamic curve of the rotation angle was obtained and then compared with the results shown in Figure 8.
As mentioned in Section 3.2, parameters α_{3}, α_{4}, α_{5}, α_{6}, α_{9}, α_{10}, α_{12}, α_{17}, α_{18}, α_{20}, α_{21}, α_{22}, and α_{23} are more sensitive to the step response than the other parameters; therefore, these parameters should be prioritized. Parameters α_{3}, α_{4}, α_{5}, α_{6}, α_{9}, α_{10}, and α_{12} are the structural parameters of the actuator, which will not change in a short time under normal operating conditions, and the sensitivity curves of parameters α_{17}, α_{22} and α_{23} in Figure 8 are exactly the same. Considering the parameters that change rapidly over time and for the convenience of expression, only parameters α_{18}, α_{20}, α_{21}, and α_{23} were selected for verification. A comparison between the theoretical and cosimulation results is shown in Figures 12, 13, 14.
As shown by the curve, although the shapes of the theoretical and experimental curves are not completely consistent owing to the effects of the contact parameters, simulation step size, or other factors, the trend and range of the curves are similar for each parameter under different input conditions. This consistency proves the accuracy of the solution results of parameter sensitivity in the previous section and shows the effectiveness of using the firstorder trajectory sensitivity analysis method to analyze the parameter sensitivity of the system. Because sensitivity analysis is used to evaluate the degree of influence of parameter variation on the system output, the slight error between the theoretical and experimental dynamic curves barely affects the analysis results. Therefore, the method proposed herein is applicable to the analysis of similar parameter sensitivity problems.
Analysis of Results
In this section, the sensitivity solution is analyzed more comprehensively. As shown in 8, the sensitivity function of each parameter changes with time. To quantify this dynamic process, a sensitivity index must first be determined. Farahat proposed four sensitivity indexes, among which the entirety index is reported to be the best index because it comprehensively considers all performance characteristics. In this study, the same index was used as the sensitivity index, and it is expressed as follows [21]:
Using Eq. (23), the curves in Figure 8 were integrated to obtain the sensitivity index values of the 23 parameters under nine operating conditions. The results are shown in Figures 15, 16, 17, where only parameters with a high sensitivity index are presented. Parameters whose sensitivity index is extremely low are omitted as their effects are negligible. The height of the column in the figure represents the integration of the absolute change in the output shaft rotation angle over the simulation time (0.3 s). Generally, the larger the height, the more sensitive is the output to the parameters.
As shown in Figures 15, 16, 17, when the system is under the same load conditions, the larger the step signal, the greater is the sensitivity index for a certain parameter. Moreover, the sensitivity index ranking of the parameters is the same when different step input signals are imposed. For the noload condition, the order from high to low based on the sensitivity index of the parameters is as follows:
The corresponding quantitative relationship is expressed as
For the 100 N·m load condition,
Meanwhile, for the 200 N·m load conditions,
As indicated in Eqs. (24)–(29), when the system is under different load conditions, the sensitivity ranking of the parameters and the numerical relationship between the parameters change. To observe the changes in various parameters under different operating conditions, the sensitivity indices of the parameters under the nine operating conditions are summarized, as shown in Figure 18.
As shown in Figure 18, the sensitivity of each parameter increases with the step signal. However, as the system load increases, the sensitivity of some parameters (including S_{1}, S_{2}, Ψ_{1}, Ψ_{1}, d_{1}, d_{2}, K_{d}, p_{s}, K_{axv}, and K_{p}) increases, whereas the sensitivity of other parameters (including A_{p}, ω, and ζ) decreases. The sensitivity of the former parameters increases significantly, whereas that the latter parameters decreases slightly. For parameters Ψ_{1}, Ψ_{2}, d_{1}, and d_{2} in particular, the order of magnitude of the sensitivity index is only 10^{−8} under the noload condition; however, under a 200 N·m load, their sensitivity index values become tens of thousands of times that of the noload condition.
Conclusions and Future Studies
In this study, a complete mathematical model of a valvecontrolled HHRA system with an angular displacement closed loop was established. Subsequently, the influence degree and law of 10% parameter change on the angular displacement step response were quantitatively obtained using the firstorder trajectory sensitivity analysis method. Finally, a prototype experiment and cosimulation were performed to verify the accuracy of the system dynamics model and sensitivity results, respectively. The good agreement between the theoretical and experimental (or cosimulation) values shows that the nonlinear system model established in this study can represent the dynamic characteristics of valvecontrolled HHRA closedloop systems effectively, and that the sensitivity equations are accurate. Therefore, the results of this study are reliable and can provide a basis for the structural parameter optimization or control compensation of similar systems. The conclusions of the sensitivity analysis are as follows:

(1)
An analysis of the sensitivity of the angular displacement closedloop system when the parameters changed by 10% showed that the sensitivity ranking and values of the parameters were different under different operating conditions. In general, under the nine operating conditions involving different step inputs and loads described herein, the perturbation of structural parameters S_{1}, S_{2}, Ψ_{1}, Ψ_{1}, d_{1}, d_{2}, and A_{p} of the HHRA, operating parameters K_{d} and p_{s}, servo valve parameters ω, ζ, and K_{axv}, and the control parameter K_{p} significantly affected the dynamic characteristics of the system. Moreover, the sensitivity of these parameters increased significantly with an increase in the step input signal. For the other parameters, the effect of smallscale perturbations was negligible.

(2)
For structural parameters with high sensitivity, sensitivity can be reduced by selecting the appropriate parameters or optimizing the structure. For operating parameters with high sensitivity and rapid perturbation, their fluctuations must be reduced when designing the system. The parameters of the servo valve are highly sensitive; therefore, the values of the valve parameters used during modeling should be the same as those of the actual system because an incorrect value may cause significant deviation between the actual situation and design requirements. The control parameters are expected to significantly affect the system output because the dynamic characteristics of the system are often altered when the controller parameters are adjusted.
In future studies, the valvecontrolled HHRA system designed in this study will be used to operate legged robots because the characteristics of helical hydraulic cylinders are suitable for highspeed robots, which require a compact structure and a high explosive force. In addition, to adapt the designed system to systems with different control performance requirements, a sensitivity analysis of the parameters of the system will be performed using different control algorithms.
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Acknowledgements
The authors sincerely thank the engineers in Xiangyang Hangyu Electromechanical Hydraulic Application Technology Co. Ltd. for their assistance in processing and experimentation.
Funding
Supported by National Natural Science Foundation of China (Grant No. 51922093), Scientific Research Fund of Zhejiang Provincial Education Department of China (Grant No. Y202148352), and Major Science and Technology Projects in Ningbo of China (Grant No. 2019B10054).
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JZ and BX were responsible for the entire trial; KZ was a major contributor in writing the manuscript; MG, HZ, XW, HH, QS assisted in procurement, experiment, etc. All authors have read and approved the final manuscript.
Authors’ Information
Kun Zhang, born in 1996, is currently a Ph.D. candidate at State Key Laboratory of Fluid Power and Mechatronic Systems, Zhejiang University, China. His research interests include hydraulic systems and robotic control.
Junhui Zhang, born in 1983, is currently deputy director at State Key Laboratory of Fluid Power and Mechatronic Systems, Zhejiang University, China. He received his Ph.D. degree from Zhejiang University, China, in 2012. His research interests include hydraulic transmissions, hydraulic components, and hydraulic robots.
Minyao Gan, born in 1978, is currently an engineer at Shanghai Marine Equipment Research Institute, China.
Huaizhi Zong, born in 1995, is currently a Ph.D. candidate at State Key Laboratory of Fluid Power and Mechatronic Systems, Zhejiang University, China. His research interests include hydraulic components and robotic design.
Ximeng Wang, born in 1997, is currently a master candidate at State Key Laboratory of Fluid Power and Mechatronic Systems, Zhejiang University, China. His research interests include electric control systems and robotic control.
Hsinpu Huang, born in 1995, is currently a master candidate at State Key Laboratory of Fluid Power and Mechatronic Systems, Zhejiang University, China. His main research interests include additive manufacturing and robotic design.
Qi Su, born in 1987, is currently an assistant research fellow at State Key Laboratory of Fluid Power and Mechatronic Systems, Zhejiang University, China. He received his Ph.D. degree from Zhejiang University, China, in 2016. His primary research interests include electromechanical systems and hydraulic valves.
Bing Xu, born in 1971, is a professor at Zhejiang University, China. He served as a director at State Key Laboratory of Fluid Power and Mechatronic Systems, Zhejiang University, China. His main research interests include hydraulic components and systems.
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Zhang, K., Zhang, J., Gan, M. et al. Modeling and Parameter Sensitivity Analysis of ValveControlled Helical Hydraulic Rotary Actuator System. Chin. J. Mech. Eng. 35, 66 (2022). https://doi.org/10.1186/s1003302200737w
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DOI: https://doi.org/10.1186/s1003302200737w
Keywords
 Helical hydraulic rotary actuator
 Dynamic model
 Closedloop system
 Sensitivity analysis
 Prototype experiment
 Cosimulation