Author:
Ivanov D,Ovchinnikov M,Tkachev S
Abstract
Abstract
The paper considers various approaches nanosatellites formation flying control, presents dynamic models of the motion of a group of nanosatellites, considers various algorithms for controlling relative angular and translational motions, taking into account the specifics of small satellites and limited inter-satellite communication capabilities. The paper discusses various approaches to the formation flying control, including those using perspective methods that do not require the fuel consumption. With a large number of spacecraft in a group, a new class of space systems appears, defined as a swarm. The main difficulty in implementing a swarm formation flying of satellites is navigation and control of the mutual relative motion of an individual satellite in a swarm, taking into account the fundamental impossibility of having information about the phase state vector of each swarm element. The features of decentralized algorithms for controlling the satellites swarm motion are considered and the dynamics of the swarm is investigated.
Reference57 articles.
1. A survey of spacecraft formation flying guidance and control (part 1): guidance;Scharf,2003
2. Survey on Guidance Navigation and Control Requirements for Spacecraft Formation-Flying Missions;Di Mauro;Journal of Guidance, Control, and Dynamics,2018
3. Maintenance of satellite formations using environmental forces vol 102;Kumar;Acta Astronautica,2014
4. Orbital formationkeeping with differential drag;Leonard;Journal of Guidance, Control, and Dynamics,1989