A hybrid control scheme for attitude and vibration suppression of a flexible spacecraft using energy-based actuators switching mechanism-Reference-Cited by-同舟云学术

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A hybrid control scheme for attitude and vibration suppression of a flexible spacecraft using energy-based actuators switching mechanism

Published:2018-11 Issue: Volume:82-83 Page:140-148
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Azimi Milad^ORCID,Sharifi Ghasem

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference36 articles.

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2. Inverse dynamics particle swarm optimization applied to constrained minimum-time maneuvers using reaction wheels;Spiller;Aerosp. Sci. Technol.,2018

3. A time suboptimal method for real-time spacecraft attitude agile maneuvering with angular velocity constraint;Wu;Proc. Inst. Mech. Eng., G J. Aerosp. Eng.,2017

4. Design and analysis of a moment control unit for agile satellite with high attitude stability requirement;Zhang;Acta Astronaut.,2016

5. Time-optimal three-axis reorientation of asymmetric rigid spacecraft via homotopic approach;Li;Adv. Space Res.,2016

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