Longitudinal flight control design with handling quality requirements
نویسندگان
چکیده
منابع مشابه
Design of a Flight Control System in Compliance with Fling and Handling Quality Requirements
The un-augmented open loop 6-DOF Aerosonde exhibits poor stability and control characteristics in compliance with MIL-F8785C flying quality standards. As in most classical fixed wing aircrafts, the control inputs to Aerosonde result in pitch, roll and yaw rate responses (rate command characteristics). This has made manual trimming of the UAV, at a given flight condition, with a human pilot-...
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ژورنال
عنوان ژورنال: The Aeronautical Journal
سال: 2006
ISSN: 0001-9240,2059-6464
DOI: 10.1017/s0001924000001494