Analytical Solutions to Two-Impulse Nondrifting Transfer Problems for Rendezvous in Elliptical Orbits

Author:

Peters Thomas V.1,Noomen Ron1,Colmenarejo Pablo1

Affiliation:

1. Advanced Systems Technologies, GMV, ES 28760 Madrid, Spain

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Reference32 articles.

1. Approach safety and collision avoidance

2. Orbit dynamics and trajectory elements

3. Di SottoE.BastanteJ. C.DraiR. “Guidance Algorithms for Non-Drifting Trajectory Generation and Control in Rendezvous Missions into Elliptical Orbits,” Proceedings of the 20th International Symposium on Space Flight Dynamics [CD-ROM], NASA CP-2007-214158, Annapolis, MD, Sept. 2007.

4. Navigating the Road to Autonomous Orbital Rendezvous

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