Solution Based on Dynamical Approach for Multiple-Revolution Lambert Problem-Reference-Cited by-同舟云学术

Solution Based on Dynamical Approach for Multiple-Revolution Lambert Problem

Published:2011-05 Issue:3 Volume:34 Page:920-923
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Arlulkar P. V.¹,Naik S. D.¹

Affiliation:

1. Defence Institute of Advanced Technology, Girinagar, Pune, Maharashtra 411 025, India

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/10.2514/1.51723

Reference10 articles.

1. Bate, R. R., Mueller, D. D., and White, J. E., Fundamentals of Astrodynamics, Dover, New York, 1971, pp.227-276.

2. An elegant Lambert algorithm

3. Loechler, L. A. "An Elegant Lambert Algorithm for Multiple Revolution Orbits," M.S. Thesis,Department of Aeronautics and Astronautics, Massachusetts Inst. of Technology, Cambridge, MA,1988.

4. A Class of Optimal Two-Impulse Rendezvous Using Multiple-Revolution Lambert Solutions

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