Application of the Delta-Rho perturbation method to autonomous orbitcomputation-Reference-Cited by-同舟云学术

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Application of the Delta-Rho perturbation method to autonomous orbitcomputation

Published:1985-03 Issue:2 Volume:8 Page:243-248
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Schneider Alan M.¹,Trexel Brian D.²

Affiliation:

1. University of California at San Diego, LaJolla, California

2. M/A COMLINKABIT, San Diego, California

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/10.2514/3.19966

Reference4 articles.

1. Delta-Rho, A perturbation method for general and astrodynamical trajectories

2. 2Leyland, J. A. "Delta-Rho, A Second-Order Trajectory Perturbation Technique," Ph.D. Thesis,Applied Mechanics and Engineering Sciences Department, Universityof California at San Diego, La Jolla, Calif.1979.

3. 3Trexel, B. "Delta-Rho, A Second-Order Trajectory Perturbation Technique for Propagating Autonomous Satellite Orbits," M.S. Thesis,Applied Mechanics and Engineering Sciences Department, Universityof California at San Diego, La Jolla, California,1984.

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. Compressed polynomial approach for onboard ephemeris representation;Journal of Guidance, Control, and Dynamics;1990-07

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