Abstract:
The task of reentry vehicle (RV) guidance at the skip trajectory after return from the Moon is considered. Some modification of reentry terminal guidance algorithm (modified) — RTGA-M is suggested. It provides two-parametric guidance during the first reentry phase entire for majority of disturbed trajectories. By statistical test of 1000 disturbed trajectories was shown efficiency of the modification.
Keywords:return from the Moon, skip trajectory, terminal guidance algorithm, reentry vehicle.