Enhanced attitude control structure for small satellites with reaction wheels
Purpose: This paper aims to describe a design enhancement for the satellite attitude control system using reaction wheels, and the wheel momentum unloading using magnetorquers. Design/methodology/approach: The proportional – integral–derivative-controller and active force control (AFC) schemes are d...
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Emerald
2015
|
| Online Access: | http://psasir.upm.edu.my/id/eprint/44624/1/Enhanced%20attitude%20control%20structure%20for%20small%20satellites%20with%20reaction%20wheels.pdf |
Search Result 1
Enhanced attitude control structure for small satellites with reaction wheels
Published 2019
Get full text
Thesis