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