抄録
On-line flight control system for aircraft with elevator failures is discussed in this paper. Flight path is generated by combining simple paths, such as horizontal paths, descending paths and circular paths. In order to track the generated optimal flight path, control input is calculated by using time-scale separated Inverse Dynamics. In this process, the adjustable horizontal stabilizer is used as a substitute for the elevator to control the aircraft with elevator failures. So, the thrust and adjustable horizontal stabilizer angle need to be calculated by the proposed cotrol law. Finally, the effectiveness of the proposed algorithm is checked in flight simulation. The flight experiment is scheduled in this autumn using MuPAL-α (Multi-Purpose Aviation Laboratory of JAXA).
