Attitude Control Synthesis for Small Satellites Using Gradient Method. Part I - Nonlinear Equations
Journal Title: INCAS BULLETIN - Year 2012, Vol 4, Issue 4
Abstract
The paper presents some aspects for synthesis of small satellites attitude control. The satellite nonlinear model presented here will be with six degrees of freedom. After movement equation linearization the stability and command matrixes will be established and the controller will be obtained using gradient and gradient method. Two attitude control cases will be analysed: the reaction wheels and the micro thrusters. The results will be used in the project European Space Moon Orbit - ESMO founded by European Space Agency in which the University POLITEHNICA of Bucharest is involved.
Authors and Affiliations
Teodor-Viorel CHELARU, Adrian-Mihail STOICA, Adrian CHELARU
Keywords
Related Articles
- EP ID EP151088
- DOI 10.13111/2066-8201.2012.4.4.5
- Views 88
- Downloads 0
Thermal Performance of Ablative/ Ceramic Composite
A hybrid thermal protection system for atmospheric earth re-entry based on ablative materials on top of ceramic matrix composites is investigated for the protection of the metallic structure in oxidative and high tempera...
Aerodynamic Interference between Oscillating Lifting Surfaces and Fuselage. Part 3: Some Applications of Oscillating Lifting Surface Theory to the Flapping Wing
Project management templates used to plan and manage product and service provision. Case study
This article presents a compilation of methods and techniques that help manage projects successfully and which are developed by IAQG - International Aerospace Quality Group. Project management is a structured process tha...
ION STROESCU (1888-1961) A MAN and A LIFE – for a passion!