Utilization of osculating elements in terminal control of spacecraft motion

Details Utilization of osculating elements in terminal control of spacecraft motion Utilization of osculating elements in terminal control of spacecraft motion

Publishing date

Sep 1975

URL

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975kosis..13..645b&link_type=abstract

Journals

Kosmicheskie Issledovaniia, vol. 13, Sept.-Oct. 1975, p. 645-650. In Russian.

Science

Astronomy and Astrophysics

Field

Astronomy

Additional info 3

Astrodynamics, Optimal Control, Orbit Perturbation, Spacecraft Control, Terminal Guidance, Trajectory Optimization, Orbit Calculation, Prediction Analysis Techniques

Type

Scientific paper

Abstract

The problem is examined of controlling the final state of a spacecraft
along powered-flight trajectories. Control is achieved by continuous
correction of the trajectory by predicting the miss at the final point.
The accuracy requirements of the prediction are discussed, and methods
of improving prediction accuracy are proposed.

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