Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
5472229 | Acta Astronautica | 2017 | 13 Pages |
Abstract
The self-organizing control strategy for asteroid intelligent detection swarm, which is considered as a space application instance of intelligent swarm, is developed. The leader-follower model for the asteroid intelligent detection swarm is established, and the further analysis is conducted for massive asteroid and small asteroid. For a massive asteroid, the leader spacecraft flies under the gravity field of the asteroid. For a small asteroid, the asteroid gravity is negligible, and a trajectory planning method is proposed based on elliptic cavity virtual potential field. The self-organizing control strategy for the follower spacecraft is developed based on a mechanism of velocity planning and velocity tracking. The simulation results show that the self-organizing control strategy is valid for both massive asteroid and small asteroid, and the exploration swarm forms a stable configuration.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Meiyan An, Zhaokui Wang, Yulin Zhang,