Gliding-Guided Projectile Attitude Tracking Controller Design Based on Improved Adaptive Twisting Sliding Mode Algorithm

Adaptive Sliding Mode Controller Design For Attitude Small UAV

Received Apr 6 , 2015 Revised Aug 18 , 2015 Accepted Aug 26 , 2015 The dynamic of Unmanned Aerial Vehicle (UAV) is nonlinear, strongly coupled, multi-input multi-output (MIMO), and subject to uncertainties and external disturbances. In this paper, an adaptive sliding mode controller (ASMC) is integrated to design the attitude control system for an inner loop fixed wing UAV. In the proposed sche...

Robust Sliding Mode Controller for Trajectory Tracking and Attitude Control of a Nonholonomic Spherical Mobile Robot

Based on dynamic modeling, robust trajectory tracking control of attitude and position of a spherical mobile robot is proposed. In this paper, the spherical robot is composed of a spherical shell and three independent rotors which act as the inner driver mechanism. Owing to rolling without slipping assumption, the robot is subjected to two nonholonomic constraints. The state space representatio...

Adaptive Backstepping Sliding Mode Control of Spacecraft Attitude Tracking

This paper investigates the attitude tracking problem for rigid spacecraft. An adaptive backstepping sliding mode control law is proposed to solve this problem in the presence of inertia uncertainties and external disturbances. The control scheme is developed by combining sliding mode control with adaptive backstepping technique to achieve fast and accurate tracking responses. The proposed cont...

On-line genetic algorithm-based fuzzy-neural sliding mode controller using improved adaptive bound reduced-form genetic algorithm

On-line genetic algorithm-based fuzzy-neural sliding mode controller using improved adaptive bound reduced-form genetic algorithm Ping-Zong Lin a , Wei-Yen Wang b , Tsu-Tian Lee c & Chi-Hsu Wang a a Department of Electrical and Control Engineering , National Chiao Tung University , Hsinchu, Taiwan b Department of Applied Electronics Technology , National Taiwan Normal University , Taipei, 106 T...

Adaptive Fuzzy Sliding-Mode Attitude Controller Design for Spacecrafts with Thrusters