Aerodynamic and gravity gradient based attitude control for CubeSats in the presence of environmental and spacecraft uncertainties
Author:
Funder
Air Force Office of Scientific Research
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference34 articles.
1. CubeSat Design Specification Rev.13,2015
2. Passive 3 axis attitude control of MSU-1 pico-satellite;Martinelli;Acta Astronaut.,2005
3. Differential-drag-based roto-translational control for propellant-less spacecraft;Pastorelli;Acta Astronaut.,2015
4. Roto-translational spacecraft formation control using aerodynamic forces;Sun;J. Guid. Control Dyn.,2017
5. Attitude control of a 2U cubesat by magnetic and air drag torques;Sutherland;IEEE Trans. Control Syst. Technol.,2019
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