This paper describes some novel flight tests and analysis techniques in the flight dynamics and handling qualities area. These techniques were utilized during the initial flight envelope clearance of the X-29A aircraft and were largely responsible for the completion of the flight controls clearance program without any incidents or significant delays. The resulting open-loop and closed-loop frequency responses and the time history comparison using flight and linear simulation data are discussed.
Dynamic stability and handling qualities tests on a highly augmented, statically unstable airplane
Society of Flight Test Engineers, Annual Symposium ; 1987 ; Amsterdam, Netherlands
1987-01-01
Conference paper
No indication
English