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THE AIRSPEED CONTROL MODULE BASED ON HEIGHT DEVIATION AND METHOD FOR CONTROLLING THE AIRSPEED BASED ON HEIGHT DEVIATION USING THE SAME MODULE
THE AIRSPEED CONTROL MODULE BASED ON HEIGHT DEVIATION AND METHOD FOR CONTROLLING THE AIRSPEED BASED ON HEIGHT DEVIATION USING THE SAME MODULE
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机译:基于高度偏差的空中控制模块以及使用相同模块的基于高度偏差的空中控制方法
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摘要
PURPOSE: An airspeed control module based on height deviation and an airspeed control method based on height deviation using the same are provided to stably control an aircraft by comparing a command height applied to the aircraft with a current height. CONSTITUTION: An airspeed control module based on height deviation processes a command speed (Hcmd) (1) according to a height error (Herr) (31) which is the difference between the command speed applied to an aircraft (10) and a current height (Hfb) (11) fed back from the aircraft. The airspeed control module outputs the processed command speed to a final command speed (Vcmd_f) (39) and inputs the outputted command speed to an aircraft control module (20) to control the airspeed of the aircraft. [Reference numerals] (10) Aircraft; (20) Control loop (altitude, speed, and pitch); (AA) Thrust command; (BB) Horizontal tail command; (CC) Speed feedback signal (V_fb); (DD) Pitch orientation angle feedback signal; (EE) Pitch angle speed feedback signal
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