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Controllability Analysis of Motion of Artificial Satellite Under the Effect of Oblateness of the Earth

2022/02/28 by Jaita Sharma, B. S. Ratanpal, Sharma, Jaita +5
Engineering · #Control and Dynamics of Mobile Robots #FOS: Mathematics #Optimization and Control (math.OC) #Space Satellite Systems and Control #Spacecraft Dynamics and Control

paper · pdf · doi:10.48550/arxiv.2203.01410

openalex publication_date 2022/02/28 · openalex created_date 2022/04/03 · openalex updated_date 2026/07/28

Abstract

In this article we have studied the controllability of artificial satellite under the effect of zonal harmonic J2 in cylindrical polar coordinates systems. Seven different cases of thrusters in various directions have been analyzed and it is found that the system is controllable if we apply thrusters in either r, θ and z or θ and z direction. The equations governing motion of satellite have been linearized and Kalman controllability test is applied to check the controllability of the system. We have also derived controller u for the linearized system. The trajectory of the system have been plotted to show the controllability of the system.

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