Trim angle of attack determination and altitude correction in the TAUS-MC algorithm
Abstract:
Algorithms for determination of actual trim angle of attack and altitude correction of inertial navigation errors are suggested. Both algorithms are a part of onboard TAUS-MC algorithm of vehicle motion control at reentry trajectories from the Moon with range of 10000 km and two atmospheric phases.
Keywords:
terminal control, reentry at return from the Moon, skip-up trajectory, trim angle of attack, errors of inertial navigation
