New State Transition Matrix for Relative Motion on an Arbitrary Elliptical Orbit
Author:
Affiliation:
1. National Space Development Agency, Tokyo 105-8060, Japan
2. European Space Research and Technology Center, 2200 AG Noordwijk, The Netherlands
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
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.4875
Reference4 articles.
1. State Transition Matrices for Terminal Rendezvous Studies: Brief Survey and New Example
2. Strategies and schemes for rendezvous on geostationary transfer orbit
3. Time-Explicit Representation of Relative Motion Between Elliptical Orbits
4. New form for the optimal rendezvous equations near a Keplerian orbit
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