Trajectory optimization by making use of the closed solution of constant thrust-acceleration motion

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1 March 1976

journal article
research article
Published by Springer Nature in Celestial Mechanics and Dynamical Astronomy

Vol. 14 (1) , 91-103
https://doi.org/10.1007/bf01247135

Abstract

No abstract available

Keywords

This publication has 5 references indexed in Scilit:

A problem of orbital dynamics, which is separable in KS-variables
Celestial Mechanics and Dynamical Astronomy, 1971
Linear and Regular Celestial Mechanics
Published by Springer Nature ,1971
A new approach to variable metric algorithms
The Computer Journal, 1970
An efficient method for calculating optimal free-space n-impulse trajectories.
AIAA Journal, 1968
3 Singular Extremals
Published by Elsevier ,1967