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Ballistic analysis of flight planning methods for spacecraft inspecting groups of objects on the geostationary orbit

Authors: Gnezdova E. K.
Published in issue: #11(28)/2018
DOI: 10.18698/2541-8009-2018-11-404


Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

Keywords: spacecraft, drift, target fly-around, geostationary orbit, planning algorithm, characteristic speed, inspection order, ballistic support, depth-first search, direct search method
Published: 15.11.2018

The analysis of flight planning methods for spacecraft inspecting groups of objects on the geostationary orbit is conducted. The analysis includes solving the problem of ballistic support for the fly-around of space object on the geostationary orbit. The flight plan includes optimal search of the optimal fly-around plan with minimum characteristic speed expenses provided that the allowable time limits are not breached. The optimal solution is done using direct search method — depth-first search with constraints imposed on the search depth and the number of tentative variants of node branching. The obtained quasi-optimal solution depends on the set node branching depth limited by the allowable computational cost.


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