Title: X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data
Subjects: Airplanes, Algorithms, Angle of attack, Angle of attack (Aerodynamics), Control systems, Directional control, Directional stability, Grumman X-29A (Jet plane), Lateral Stability of airplanes, Lateral control, Lateral stability, Parameter identification, Research aircraft, X-29 aircraft, Yawing (Aerodynamics)