TY - JOUR
T1 - Estimation-enhanced disturbance-observer-based discrete sliding mode control of constrained dual-arm space robots
AU - Li, Yi
AU - Yue, Xiaokui
AU - Zhang, Teng
N1 - Publisher Copyright:
© 2026 Elsevier Masson SAS.
PY - 2026/12
Y1 - 2026/12
N2 - High-precision trajectory control of dual-arm space robots remains challenging when the two manipulators firmly grasp a common target. In this case, the resulting closed-chain constraints tightly couple the base, manipulators, and payload, while external disturbances, measurement noise, and actuator saturation jointly degrade closed-loop performance. This paper proposes an estimation-enhanced disturbance-observer-based discrete integral sliding mode control scheme for constrained dual-arm space robots. The key idea is to combine constraint-consistent state reconstruction with disturbance compensation so that robust high-precision control can be achieved under practical sensing and actuation limitations. First, the closed-chain dynamics are reformulated via the embedding technique, yielding a reduced constrained model suitable for controller and observer synthesis. Second, a constrained extended Kalman filter is introduced to reconstruct reliable states from noisy measurements while preserving kinematic consistency. Third, a second-order disturbance observer is designed on the reduced constrained dynamics to estimate lumped disturbances and provide feedforward compensation. On this basis, a discrete integral sliding mode controller with an anti-saturation auxiliary system is developed to improve tracking accuracy, disturbance rejection, and transient behavior under bounded torque inputs. Lyapunov analysis proves that the closed-loop tracking errors are uniformly ultimately bounded under bounded state-estimation, disturbance-observation, and projected saturation residuals. Comparative simulations, Monte Carlo tests, and sensitivity analyses show that the proposed framework achieves smaller tracking errors, faster convergence, and stronger disturbance rejection than benchmark methods.
AB - High-precision trajectory control of dual-arm space robots remains challenging when the two manipulators firmly grasp a common target. In this case, the resulting closed-chain constraints tightly couple the base, manipulators, and payload, while external disturbances, measurement noise, and actuator saturation jointly degrade closed-loop performance. This paper proposes an estimation-enhanced disturbance-observer-based discrete integral sliding mode control scheme for constrained dual-arm space robots. The key idea is to combine constraint-consistent state reconstruction with disturbance compensation so that robust high-precision control can be achieved under practical sensing and actuation limitations. First, the closed-chain dynamics are reformulated via the embedding technique, yielding a reduced constrained model suitable for controller and observer synthesis. Second, a constrained extended Kalman filter is introduced to reconstruct reliable states from noisy measurements while preserving kinematic consistency. Third, a second-order disturbance observer is designed on the reduced constrained dynamics to estimate lumped disturbances and provide feedforward compensation. On this basis, a discrete integral sliding mode controller with an anti-saturation auxiliary system is developed to improve tracking accuracy, disturbance rejection, and transient behavior under bounded torque inputs. Lyapunov analysis proves that the closed-loop tracking errors are uniformly ultimately bounded under bounded state-estimation, disturbance-observation, and projected saturation residuals. Comparative simulations, Monte Carlo tests, and sensitivity analyses show that the proposed framework achieves smaller tracking errors, faster convergence, and stronger disturbance rejection than benchmark methods.
KW - Constrained extended Kalman filter
KW - Discrete sliding mode control
KW - Disturbance observer
KW - Dual-arm space robot
KW - High-precision control
UR - https://www.scopus.com/pages/publications/105046981741
U2 - 10.1016/j.ast.2026.113478
DO - 10.1016/j.ast.2026.113478
M3 - 文章
AN - SCOPUS:105046981741
SN - 1270-9638
VL - 179
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 113478
ER -