Spacecraft Formation Guidance Law using a State Transition Matrix With Gravitational, Drag and Third-Body Perturbations
Author:
Affiliation:
1. Carleton University
Publisher
American Institute of Aeronautics and Astronautics
Reference37 articles.
1. Mission analysis for PROBA-3 nominal operations
2. Terminal Guidance System for Satellite Rendezvous
3. Relative Dynamics and Control of Spacecraft Formations in Eccentric Orbits
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2. Software-in-the-Loop Validation of a Novel Two-Point Optimal Guidance for Perturbed Spacecraft Rendezvous and Formations;The Journal of the Astronautical Sciences;2023-10-04
3. Hybrid Guardian Map-based adaptive control of spacecraft formation flying on highly elliptical orbits in the restricted three-body problem;Acta Astronautica;2021-03
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