Desired trajectory and guidance force generators for an aircraft
Author:
Affiliation:
1. National Defense Academy, Yokosuka, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-3873
Reference11 articles.
1. Aircraft automatic flight control system with model inversion
2. Jackson,J.flf. Crouch, P.E. "Dynamic Interpolation and Application to Flight Control", 1.Guidance, Vol.14, No.4,1991,pp.814-822.
3. Inverse and optimal control for precision aerobatic maneuvers
4. Menon,P.K.A., Badgett,M.E. and lalker,R.A. "Nonlinear Flight Test Trajectory Controllers for Aircraft". 1.Guidance, 10-1(1987). pp.67-72.
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