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Solar System Research

, Volume 52, Issue 7, pp 613–621 | Cite as

Use of Programs for Two-Parameter Multiple Impulse Correction of Altitude and Inclination of Circular Orbits

  • A. E. NazarovEmail author
Article
  • 7 Downloads

Abstract

The paper describes the method for the development of programs for two-parameter multiple impulse correction of altitude and inclination of circular orbits. The considered corrections feature the simultaneous adjustment of altitude and inclination of the orbit under limited thrust of the propulsion system of the spacecraft. Low thrust-to-weight ratio of the spacecraft leads to the need for a correction program consisting of several burns of the propulsion system. Thrust vector orientation, burn time, and its operation duration are determined as propulsion system parameters.

Keywords

orbit correction spacecraft propulsion system circular orbit 

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Copyright information

© Pleiades Publishing, Inc. 2018

Authors and Affiliations

  1. 1.Lavochkin AssociationKhimki, Moscow oblastRussia

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