Nonlinear adaptive trajectory tracking control for a quad-rotor with parametric uncertainty

被引:23
|
作者
Sun, Liang [1 ]
Zuo, Zongyu [1 ]
机构
[1] Beijing Univ Aeronaut & Astronaut, Res Div 7, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
Quad-rotor control; trajectory tracking; nonlinear adaptive control; noncertainty equivalence principle; command filter; COMMAND-FILTERED COMPENSATION; ATTITUDE REPRESENTATIONS; QUADROTOR HELICOPTER; CONTROL DESIGN; FLIGHT CONTROL; SYSTEMS; INVARIANCE; SPACECRAFT; IMMERSION; VEHICLES;
D O I
10.1177/0954410014558692
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A novel adaptive control algorithm to trajectory tracking control problem for a quad-rotor with uncertain mass and inertial parameters is presented based on the noncertainty equivalence principle. The estimation laws for quad-rotor mass and inertial parameters are developed with the introduction of stable attracting manifolds into the position-loop and attitude-loop adaptation process, respectively. The position and attitude trajectory tracking control algorithms are constructed through a unified immersion and invariance adaptive control technology. With extracting the desired attitude trajectory from the position-loop, the desired attitude trajectory for the attitude-loop is calculated from a command filter. The ultimately uniformly boundedness of the closed-loop system signals is derived for the quad-rotor under the proposed control algorithm. Simulation results demonstrate the performance of the proposed approach.
引用
收藏
页码:1709 / 1721
页数:13
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