Spacecraft and Rockets
Аuthors
1*, 2*, 2*, 2**1. ,
2. Moscow Experimental Design Bureau “Mars”, 1-st Shemilovsky lane 16, building 2, Moscow, 127473, Russia
*e-mail: office@mars-mokb.ru
**e-mail: mbtch@rambler.ru
Abstract
Distinctive features of Breeze-M as a controlled object for flight control system and design philosophy of terminal control for launching it on specified orbit are examined in this work. Such control system is realized on periodic solution of boundary-value problem with numerical and analytical procedures. The applied algorithm provides high methodical precision.Keywords:
upper-stage rocket vehicle, control system, terminal control, boundary-value problem
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