Analytic solutions for intermediate-thrust arcs of rocket trajectories in a Newtonian field-Reference-Cited by-同舟云学术

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Analytic solutions for intermediate-thrust arcs of rocket trajectories in a Newtonian field

Published:1996-01 Issue:3 Volume:60 Page:421-427
ISSN:0021-8928
Container-title:Journal of Applied Mathematics and Mechanics
language:en
Short-container-title:Journal of Applied Mathematics and Mechanics

Author:

Azimov D.M.

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials,Modeling and Simulation

Reference9 articles.

1. Optimum Trajectories for Space Navigation;Lawden,1964

2. The problem of determining the trajectories in a Newtonian field;Azizov,1984

3. Optimality of intermediate-thrust arcs of rocket trajectories;Robbins;AIAA J.,1965

4. A supplement to Lawden's theory;Zavalishchin;Priki. Mat. Mekh.,1989

5. The use of the Levi-Civita method to analyse optimum trajectories;Azizov;Kosmich. Issledovaniya,1979

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