Energy optimal attitude control of a satellite actuated by magnetorquers in minimum time*
Author:
Affiliation:
1. NTNU Norwegian University of Science and Technology,Centre for Autonomous Marine Operations and Systems,Department of Engineering Cybernetics,Trondheim,Norway,NO-7491
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10252164/10252092/10252289.pdf?arnumber=10252289
Reference26 articles.
1. Energy optimal attitude control for a solar-powered spacecraft
2. Time-optimal magnetic attitude control for small spacecraft
3. Task scheduling for optimal power management and quality-of-service assurance in CubeSats
4. Energy Optimal Attitude Control and Task Execution for a Solar-Powered Spacecraft;kristiansen,2023
5. Time optimal attitude control for a rigid body
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