Application and Flight Test of Linearizing Transformations Using Measurement Feedback to the Nonlinear Control ProblemNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991 - Airplanes - 51 pages |
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accelerometer output aerodynamic aerodynamic models aircraft altitude commanded altitude rate ancom angle of attack angle-of-attack command Anz.com apparent linear system body axis command equation commanded incremental load Control Inverse Transformation control law computer control loop cos a cos deg/sec derived Euler angles excess-thrust windup turn flight data Flight-Test Results flight-test trajectory control ft/sec FTTC h.com hcom href incremental load factor inertial inverse linearizing transformation Inverse Transformation Equations kinematic acceleration level acceleration linear control law linearizing transformation equation Mach Number Command maneuver End maneuver measurement equation measurement feedback Meyer mg(cos noise nonlinear system outer-loop control Pcom Pitch Control pseudocontrol pushover-pullup maneuver qcom ramp RAV system real nonlinear control roll control roll rate shown in equation shown in figure simulated maneuver techniques throttle command thrust model time-scale separation tracking trajectory control problem vector Vref WT-map XTest z-body