A Constrained Control Allocation and Tuning Scheme for Hybrid Actuators in Spacecraft Attitude Control-Reference-Cited by-同舟云学术

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A Constrained Control Allocation and Tuning Scheme for Hybrid Actuators in Spacecraft Attitude Control

Published:2023 Issue:2 Volume:56 Page:11273-11280
ISSN:2405-8963
Container-title:IFAC-PapersOnLine
language:en
Short-container-title:IFAC-PapersOnLine

Author:

Grøtte Mariusz E.,Gravdahl J. Tommy,Johansen Tor A.

Publisher

Elsevier BV

Subject

General Medicine

Reference19 articles.

1. Time-optimal three-axis reorientation of a rigid spacecraft;Bilimoria;Journal of Guidance, Control, and Dynamics,1993

2. Evaluation of optimization methods for control allocation;Bodson;Journal of Guidance, Control, and Dynamics,2002

3. Fault tolerant control allocation using unknown input observers;Cristofaro;Au-tomatica,2014

4. Minimum-time reorientation of a rigid body;Fleming;Journal of Guidance, Control, and Dynamics,2010

5. Spacecraft attitude and angular rate tracking using reaction wheels and magnetorquers;Grøtte;IFAC-PapersOnLine,2020

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