Development of a Brute Force Method to Solve for Static and Dynamic Constrained Attitude Maneuver

Ahmad Bataineh; Ahmad Fares; Ahmad Bani Younes; Wafa Batayneh

doi:10.15866/irease.v16i5.24072

Development of a Brute Force Method to Solve for Static and Dynamic Constrained Attitude Maneuver

Ahmad Bataineh^(1*), Ahmad Fares⁽²⁾, Ahmad Bani Younes⁽³⁾, Wafa Batayneh⁽⁴⁾

^(*) Corresponding author

Authors' affiliations

DOI: https://doi.org/10.15866/irease.v16i5.24072

Abstract

In this paper, straightforward and efficient brute force method is developed to slew spacecraft in the presence of static and dynamic constrained regions. Fuzzy logic is utilized to develop a fuzzy based controller that is used to control the maneuvers and test the proposed method. The controller performance is first tested in an unconstrained attitude maneuvers and then it is utilized to test the proposed method. The spacecraft is assumed to be a 3U CubeSat and the results show through Monte Carlo simulations that the controller has successfully avoided the undesired static and dynamiccelestial objects. The proposed method inherits its simplicity from the geometric approach and has the ability to monitor continuously the constraints and it shows that the proposed method works in the presence of multiple constraints.
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Keywords

Attitude Control; Constrained Attitude; Fuzzy; Static; Dynamic; Spacecraft

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