Orbit transfer error analysis for multiple finite perigee burn, ascent trajectories

Details Orbit transfer error analysis for multiple finite perigee burn, ascent trajectories Orbit transfer error analysis for multiple finite perigee burn, ascent trajectories

Aug 1986

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1986asdy.conf...37a&link_type=abstract

IN: Astrodynamics 1985; Proceedings of the Conference, Vail, CO, August 12-15, 1985. Part 1 (A86-43201 20-12). San Diego, CA, Un

Statistics

Applications

Burning Time, Error Analysis, Pas, Trajectory Control, Transfer Orbits, Earth Orbital Environments, Kepler Laws

Scientific paper

A new algorithm has been developed which calculates the propagation of guidance and navigation errors along a nominal trajectory involving finite-duration perigee burns. A numerical simulation of a transfer from low earth orbit to geostationary orbit (including finite-duration burns, coast phases, impulsive trim burns, and an impulsive plane change and circularization burn at apogee) serves to demonstrate the applications of the algorithm. This example also indicates the effects of mid-course corrections on the final errors at apogee.

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