Use of Cartesian-Coordinate Calibration for Satellite Relative-Motion Control-Reference-Cited by-同舟云学术

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Use of Cartesian-Coordinate Calibration for Satellite Relative-Motion Control

Published:2015-09 Issue:9 Volume:38 Page:1842-1847
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Sinclair Andrew J.¹,Sherrill Ryan E.²,Lovell T. Alan³

Affiliation:

1. Aerospace Engineering Department, Auburn University, Auburn, Alabama 36849

2. Engineering & Program Management Group, Engility Corporation, Eglin Air Force Base, Florida 32542

3. Air Force Research Laboratory, Space Vehicles Directorate, Kirtland Air Force Base, New Mexico 87117

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/10.2514/1.G000683

Reference19 articles.

1. Lambert's Problem Revisited

2. Space guidance evolution - A personal narrative

3. An Introduction to the Mathematics and Methods of Astrodynamics, Revised Edition

4. also Advances in the Astronautical Sciences, Vol. 148, Univelt, Inc., San Diego, CA, 2013, pp. 4071–4086.

5. Calibration of Linearized Solutions for Satellite Relative Motion

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Coordinate‐Invariant Linear Quadratic Control;PAMM;2019-11

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