Fixed-Time Attitude Tracking Control for Rigid Spacecraft Without Angular Velocity Measurements

被引：0
|
作者：
Zou, An-Min [1 ]
Fan, Zhun [1 ,2 ,3 ]
机构：
[1] Shantou Univ, Coll Engn, Dept Elect & Informat Engn, Guangdong Prov Key Lab Digital Signal & Image Pro, Shantou 515063, Peoples R China
[2] Shantou Univ, Key Lab Intelligent Mfg Technol, Minist Educ, Shantou 515063, Peoples R China
[3] Huazhong Univ Sci & Technol, State Key Lab Digital Mfg Equipment & Technol, Wuhan 430074, Peoples R China
来源：
IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS | 2020年 / 67卷 / 08期
关键词：
Attitude control; fixed-time control; homogeneity property; rigid spacecraft; FINITE-TIME; OUTPUT-FEEDBACK; LYAPUNOV FUNCTION; STABILIZATION; OBSERVER; INTEGRATOR; DESIGN;
D O I：
10.1109/TIE.2019.2937035
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
This article considers the problem of velocity-free fixed-time attitude tracking control for rigid spacecraft. With the help of the homogeneity theorem, a semiglobal observer is introduced to estimate the unmeasured angular velocities within fixed time. Then, a velocity-free attitude tracking controller is designed to make the spacecraft attitude track a time-varying reference signal in finite time, which can be up bounded by a fixed number regardless of the initial conditions. Finally, numerical examples are provided to illustrate the efficiency of the present control scheme.
引用
收藏
页码：6795 / 6805
页数：11
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