Orbit Estimation of a Continuously Thrusting Spacecraft Using Variable Dimension Filters-Reference-Cited by-同舟云学术

Orbit Estimation of a Continuously Thrusting Spacecraft Using Variable Dimension Filters

Published:2015-12 Issue:12 Volume:38 Page:2407-2420
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Goff Gary M.¹,Black Johnathan T.¹,Beck Joseph A.²

Affiliation:

1. Aerospace Engineering, U.S. Air Force Institute of Technology, Wright–Patterson Air Force Base, Ohio 45433

2. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

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.G001091

Reference42 articles.

1. National Research Council, Continuing Kepler’s Quest: Assessing Air Force Space Command’s Astrodynamics Standards, The National Academies Press, Washington, D.C., 2012, pp. 38–39, http://www.nap.edu/catalog/13456/continuing-keplers-quest-assessing-air-force-space-commands-astrodynamics-standards [retrieved 1 Oct. 2012].

2. Recursive Bias Estimation and Orbit Determination

3. Orbit Determination with Improved Covariance Fidelity, Including Sensor Measurement Biases

4. WieselW. E., Modern Orbit Determination, Aphelion Press, Beavercreek, OH, 2003, pp. 93–104.

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