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Cosmic Research

, Volume 54, Issue 6, pp 483–490 | Cite as

Orbital and angular motion construction for low thrust interplanetary flight

  • R. V. Yelnikov
  • Y. V. MashtakovEmail author
  • M. Yu. Ovchinnikov
  • S. S. Tkachev
Article
  • 38 Downloads

Abstract

Low thrust interplanetary flight is considered. Firstly, the fuel-optimal control is found. Then the angular motion is synthesized. This motion provides the thruster tracking of the required by optimal control direction. And, finally, reaction wheel control law for tracking this angular motion is proposed and implemented. The numerical example is given and total operation time for thrusters is found. Disturbances from solar pressure, thrust eccentricity, inaccuracy of reaction wheels installation and errors of inertia tensor are taken into account.

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Copyright information

© Pleiades Publishing, Ltd. 2016

Authors and Affiliations

  • R. V. Yelnikov
    • 1
  • Y. V. Mashtakov
    • 2
    Email author
  • M. Yu. Ovchinnikov
    • 2
  • S. S. Tkachev
    • 2
  1. 1.Research Institute of Applied Mechanics and ElectrodynamicsMoscowRussia
  2. 2.Keldysh Institute of Applied Mathematics of RASMoscowRussia

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