FLY AROUND MISSION IN NON- KEPLERIAN ORBIT | ||||
| The International Conference on Applied Mechanics and Mechanical Engineering | ||||
| Article 21, Volume 15, 15th International Conference on Applied Mechanics and Mechanical Engineering., May 2012, Page 1-9 PDF (249.83 K) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/amme.2012.36918 | ||||
 View on SCiNiTO | ||||
| Author | ||||
| A. Badawy | ||||
| Egyptian Armed Forces. | ||||
| Abstract | ||||
| ABSTRACT On-orbit manoeuvring in Low earth non-Keplerian orbit is discussed. High performance control strategies are required for these types of formation flying missions. The simple solution for Keplerian orbit is somewhat far from accuracy, while accurate solution for non-Keplerian orbit is not simple. Motion planning algorithms are used herein to accomplish successful fly around of orbiting objects. Close manoeuvres are performed as these manoeuvring objects approach the central body around which they will fly. | ||||
| Keywords | ||||
| Space robotics; ISS; superquadric; potential field method; quaternions; motion planning | ||||
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