Continuous leaderless synchronizatn control cf multiple spacecraft on SO(3)

被引：7
作者：
Chen, Ti [1 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Nanjing 211106, Peoples R China
来源：
ASTRODYNAMICS | 2021年 / 5卷 / 03期
基金：
中国国家自然科学基金;
关键词：
leaderless synchronization; distributed observer; SO(3); adaptive controller; FLEXIBLE SPACECRAFT; DISTRIBUTED ATTITUDE; TRACKING CONTROL; SPANNING-TREES; RIGID BODIES; CONSENSUS; STABILIZATION; DYNAMICS; ACTUATOR; MOTION;
D O I：
10.1007/s42064-021-0108-y
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper presents a solution to the leaderless consensus of multiple spacecraft on SO(3) under a connected undirected graph. An algorithm is proposed to generate an undirected tree graph from a connected undirected communication topology. A distributed observer is designed to estimate the desired attitude and angular velocity for each spacecraft under the generated tree graph. An adaptive controller with a general connected undirected graph is developed to complete the synchronization task. Cases with zero and nonzero final angular velocities are considered. Theoretical proofs and numerical simulations are presented to demonstrate the effectiveness of the proposed controllers.
引用
收藏
页码：279 / 291
页数：13
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