Terminal Control Algorithm for Descent from Near-Earth Orbit with Landing in Given Region
The reentry vehicle control for descent from near-Earth orbit under significant disturbances is considered. The method of automatically shift of de-orbit point as well as adaptation to real motion conditions and modification of reference roll function to satisfy given restrictions on landing accuracy, load factor and propellant consumption are suggested. The landing within restricted region of Russian Federation is provided.
terminal control, descent from near-Earth orbit, adaptation, load factor and propellant reduce, landing within restricted region