Abstract
The reentering capsule with super-orbital velocity in manned space flight missions such as return from the lunar orbit, or from asteroids require lifting entry in order to restrict deceleration and heat transfer rate within a given range. Generally, the reentry vehicle (RV) is de-orbited by delta-V of service module etc. (SM). For the safety of the RV, entry region is desired to be far away from SM so that the any survived orbital debris of SM would never hit RV. In the process of research activities on the synthetic analysis of the skip entry of the lifting-flight capsule with super-orbital velocity, the present paper analysis introduces sensor models with noise superimposed on the true value, and the state-estimation by Kalman filtering method. Especially the effect of the attitude motion during the bank-control on the control errors is quantitatively estimated.
