Flight test maneuvers are specified for the F-18 High Alpha Research Vehicle (HARV). The maneuvers were designed for closed loop parameter identification purposes, specifically for longitudinal and lateral linear model parameter estimation at 5, 20, 30, 45, and 60 degrees angle of attack, using the NASA 1A control law. Each maneuver is to be realized by the pilot applying square wave inputs to specific pilot station controls. Maneuver descriptions and complete specifications of the time/amplitude points defining each input are included, along with plots of the input time histories.
Piloted Parameter Identification Flight Test Maneuvers for Closed Loop Modeling of the F-18 High Alpha Research Vehicle (HARV)
1996
36 pages
Report
Keine Angabe
Englisch
Aircraft , Aeronautics , Angle of attack , F-18 aircraft , Feedback control , Flight tests , Lateral control , Longitudinal control , Manual control , Parameter identification , Research aircraft , Flight control , Aircraft maneuvers , Control sticks , Control systems design , Controllability , Dynamic models , Dynamic programming , Square waves , Time dependence