Hybrid Cartesian and Orbit Element Feedback Law for Formation Flying Spacecraft
Author:
Affiliation:
1. ORION International Technologies, Albuquerque, New Mexico 87106
2. Texas A&M University, College Station, Texas 77843
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/10.2514/2.4893
Reference18 articles.
1. State Transition Matrices for Terminal Rendezvous Studies: Brief Survey and New Example
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