摘要: The flight test results obtained recently (1984) by CALSPAN on pitch-rate flight control systems in the flared landing task, obtained with the Total In-Flight Simulator (TIPS), were analyzed. The analysis approach considered is ba... 展开 The flight test results obtained recently (1984) by CALSPAN on pitch-rate flight control systems in the flared landing task, obtained with the Total In-Flight Simulator (TIPS), were analyzed. The analysis approach considered is based on the Optimal Control/Frequency Domain (OC/FD) techniques. These techniques originally stem from an optimal-control approach to perform a Neal-Smith-like analysis on aircraft attitude dynamics, but were extended and used successfully to analyze the flared landing task. 收起