Aerospace Instrument-Making Annotation << Back To a question of regimes combining of spacecraft orientation and orbit correction. M.V. Levsky Questions of the optimal combining of orientation’s and correction’s regimes at control of spacecraft motion are considered. Not only the general approaches to the solution of the specified problem but also concrete set of a task of jointed control for turn of spacecraft and its trajectory motion are investigated. The original algorithm of spacecraft’s reorientation control combined with orbit correction as applied to orbital stations is presented. High efficiency of orientation mode matching of spacecraft and maintenance of orbit altitude is demonstrated. The results of mathematical simulation for two schemes of mounting of control engines are submitted, and estimations of efficiency index and the value of correcting velocity that can be received by realization of the fixed number of turns are given.