Anti-disturbance autopilot design for missile system via finite time integral sliding mode control method and nonlinear disturbance observer technique

作者：Liu, Xinge; Liu, Zaozhen; Shan, Jiayuan; Sun, Haibin^*

来源：TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL, 2016, 38(6): 693-700.

DOI：10.1177/0142331215603793

• missile system
• autopilot design
• finite time integral sliding mode control
• nonlinear disturbance observer
• multiple disturbances

In this paper, a composite anti-disturbance autopilot design for a missile system is proposed based on finite time integral sliding mode control scheme and nonlinear disturbance observer technique. First, a nonlinear disturbance observer is developed to estimate the external disturbances with partial known information. Second, in order to obtain good disturbance rejection performance and reject the other type of disturbances, a finite time integral sliding mode control strategy is employed to the design of a feedback controller. Third, an improved adaptive composite anti-disturbance autopilot is given to avoid the inaccuracy of the upper bound of external disturbances. Finally, simulation results are employed to demonstrate the effectiveness of the proposed method.

• 出版日期2016-6
• 单位曲阜师范大学; 北京理工大学