论文信息 - A Scheme of Integrated Guidance/Autopilot Design for UAV Based on TSM Control

A Scheme of Integrated Guidance/Autopilot Design for UAV Based on TSM Control

A scheme for integrated guidance/autopilot design for some UAV based on terminal sliding-mode (TSM) control is proposed. Firstly, the terminal sliding mode control is introduced, then a guidance/control law is designed based on TSM control and the backstepping idea when an integrated guidance/autopilot model on the yaw plane of some UAV is formulated. Secondly, for the unavailable information of the maneuvering target, an estimating method is given and an auxiliary control based on a sliding mode estimator is used to offset the estimation error. Finally, a simulation of some UAV against high maneuvering targets on the yaw plane was made to verify the effectiveness and rightness of the scheme, and the simulation results have shown that good offensive performance can be got.

Jin-yong Yu | Qing-jiu Xu | Guo-rong Zhao | Ru-chuan Zhang

[1] Neil F. Palumbo,et al. Integrated missile guidance and control: a state dependent Riccati differential equation approach , 1999, Proceedings of the 1999 IEEE International Conference on Control Applications (Cat. No.99CH36328).

[2] Zhiyong Yang,et al. Novel fast adaptive terminal sliding mode controller for cross beam system , 2004, Fifth World Congress on Intelligent Control and Automation (IEEE Cat. No.04EX788).

[3] Xinghuo Yu,et al. Model reference adaptive control systems with terminal sliding modes , 1996 .

[4] I. Yaesh,et al. Optimum guidance with a single uncertain time lag , 1995 .

[5] In-Joong Ha,et al. A Lyapunov-like approach to performance analysis of 3-dimensional pure PNG laws , 1994 .

[6] Xinghuo Yu,et al. Terminal sliding mode control of MIMO linear systems , 1997 .

[7] I. G. Sarma,et al. Switched bias proportional navigation for homing guidance against highly maneuvering targets , 1994 .

[8] Di Zhou,et al. Adaptive Sliding-Mode Guidance of a Homing Missile , 1999 .