Attitude Synchronization of a Spacecraft Formation Without Velocity Measurement

被引：13

作者：

Abdessameud, A. ^{[1
]}

Tayebi, A. ^{[1
]}

机构：

[1] Univ Western Ontario, Dept Elect & Comp Engn, London, ON, Canada

来源：

47TH IEEE CONFERENCE ON DECISION AND CONTROL, 2008 (CDC 2008) | 2008年

关键词：

D O I：

10.1109/CDC.2008.4738745

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

We consider the quaternion-based attitude synchronization problem of multiple spacecraft without velocity measurements. First, we propose a leader-follower-type control scheme for the attitude synchronization of a spacecraft formation to a desired constant attitude (available only to a single spacecraft called the leader), while maintaining the same attitude during formation maneuvers. Second, we consider the consensus seeking problem, where, no reference attitude is specified, and all spacecraft are required to align their attitudes with the same (possibly time varying) final angular velocity. The communication flow between spacecraft is assumed to be bidirectional. Simulation results of a scenario of four spacecraft are provided to show the effectiveness of the proposed control scheme.

引用

页码：3719 / 3724

页数：6

共 50 条

[41] Adaptation of consensus penalty terms for attitude synchronization of spacecraft formation with unknown parameters
Zhang, Kewen
Demetriou, Michael A.
[J]. 2013 IEEE 52ND ANNUAL CONFERENCE ON DECISION AND CONTROL (CDC), 2013, : 5491 - 5496
[42] Delay Depending Decentralized Adaptive Attitude Synchronization Tracking Control of Spacecraft Formation
ZHOU Jiakang
[J]. Chinese Journal of Aeronautics, 2012, (03) : 406 - 415
[43] Inertial vector measurements based attitude synchronization control for multiple spacecraft formation
Zheng, Zhong
Shen, Mouquan
[J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 93
[44] Decentralized Fixed-Time Attitude Synchronization Control or Spacecraft Formation Flying
Sui, Weishun
Duan, Guang-Ren
Zhang, Maorui
[J]. 2018 IEEE CSAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2018,
[45] Delay Depending Decentralized Adaptive Attitude Synchronization Tracking Control of Spacecraft Formation
ZHOU Jiakang MA Guangfu HU Qinglei Department of Control Science and Engineering Harbin Institute of Technology Harbin China
[J]. Chinese Journal of Aeronautics, 2012, 25 (03) - 415
[46] ADAPTIVE SET STABILIZATION OF THE ATTITUDE OF A RIGID SPACECRAFT WITHOUT ANGULAR VELOCITY MEASUREMENTS
Ding, Shihong
Li, Shihua
Li, Qi
[J]. JOURNAL OF SYSTEMS SCIENCE & COMPLEXITY, 2011, 24 (01) : 105 - 119
[47] Adaptive set stabilization of the attitude of a rigid spacecraft without angular velocity measurements
Shihong Ding
Shihua Li
Qi Li
[J]. Journal of Systems Science and Complexity, 2011, 24 : 105 - 119
[48] Attitude stabilization of a flexible spacecraft under disturbance without angular velocity measurements
Beijing Institute of Control Engineering, Beijing 100190, China
不详
[J]. Yuhang Xuebao, 2009, 3 (1011-1016):
[49] Bounded attitude stabilization of rigid bodies without attitude estimation and velocity measurement
Guerrero-Castellanos, J. F.
Rifai, H.
Marchand, N.
Poulin, G.
[J]. 2008 IEEE INTERNATIONAL CONFERENCE ON ROBOTICS AND BIOMIMETICS, VOLS 1-4, 2009, : 2203 - +
[50] Adaptation and optimization of the synchronization gains in the adaptive spacecraft attitude synchronization
Zhang, Kewen
Demetriou, Michael A.
[J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 46 : 116 - 123

← 1 2 3 4 5 →