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Distributed finite-time attitude regulation for multiple rigid spacecraft via bounded control
- Source :
- Information Sciences. 328:144-157
- Publication Year :
- 2016
- Publisher :
- Elsevier BV, 2016.
-
Abstract
- The problem of finite-time attitude regulation for multiple rigid spacecraft with leader-follower architecture is studied. The desired attitude for spacecraft formation is represented by the attitude of a leader. A distributed finite-time convergent observer is first proposed to estimate the leader's attitude in a finite time. By using the technique of finite-time saturation control, a bounded finite-time attitude controller is designed to track the estimated attitude and then the leader's attitude in a finite time. A simulation example is finally given.
- Subjects :
- 0209 industrial biotechnology
Information Systems and Management
Observer (quantum physics)
Computer science
Control (management)
02 engineering and technology
Theoretical Computer Science
Attitude control
020901 industrial engineering & automation
0203 mechanical engineering
Artificial Intelligence
Control theory
Orbit Attitude and Maneuvering System
020301 aerospace & aeronautics
ComputingMilieux_THECOMPUTINGPROFESSION
Spacecraft
business.industry
Physics::Physics Education
Computer Science::Computers and Society
Computer Science Applications
ComputingMilieux_GENERAL
Control and Systems Engineering
Bounded function
Finite time
business
Software
Subjects
Details
- ISSN :
- 00200255
- Volume :
- 328
- Database :
- OpenAIRE
- Journal :
- Information Sciences
- Accession number :
- edsair.doi...........62513aa3fa0262c643678264b709c1ba