Attitude synchronization control for a group of flexible spacecraft

To solve the problem of attitude synchronization for a group of flexible spacecraft during formation maneuvers, a distributed attitude cooperative control strategy is investigated in this paper. Based on the backstepping design and the neighbor-based design rule, a distributed attitude control law i...

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Veröffentlicht in:Automatica (Oxford) 2014-02, Vol.50 (2), p.646-651
Hauptverfasser: Du, Haibo, Li, Shihua
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description To solve the problem of attitude synchronization for a group of flexible spacecraft during formation maneuvers, a distributed attitude cooperative control strategy is investigated in this paper. Based on the backstepping design and the neighbor-based design rule, a distributed attitude control law is constructed step by step. Using cascaded systems’ theory and graph theory, it is shown that the attitude synchronization is achieved asymptotically and the induced vibrations by flexible appendages are simultaneously suppressed under the proposed control law.
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subjects Adaptative systems
Applied sciences
Asymptotic properties
Attitude synchronization
Computer science
control theory
systems
Computer systems and distributed systems. User interface
Control system synthesis
Control theory. Systems
Design engineering
Distributed control
Exact sciences and technology
Flexible spacecraft
Fundamental areas of phenomenology (including applications)
Law
Physics
Software
Solid dynamics (ballistics, collision, multibody system, stabilization...)
Solid mechanics
Strategy
Synchronism
Synchronization
Vibration
title Attitude synchronization control for a group of flexible spacecraft
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