Ineverse dynamics approach for real-time determination of feasible aircraft reference trajectories

24th Atmospheric Flight Mechanics Conference

Volumn , Issue , 1999, Pages 545-554

  Verma, Ajay ^a   Junkins, John L ^a  

^a Department of Electrical and Computer Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; DEGREES OF FREEDOM (MECHANICS); DYNAMICS; FUNCTIONS; INVERSE PROBLEMS;

AGGRESSIVE MANEUVERS; AIRCRAFT TRAJECTORY; CONTROL REQUIREMENTS; NUMBER OF ACTUATORS; REFERENCE TRAJECTORIES; TRAJECTORY PARAMETERS; UNDER-ACTUATED SYSTEMS; UNINHABITED AERIAL VEHICLE;

TRAJECTORIES;

EID: 84960472126     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. Fliess, M., Levine, J., Matin P., Rouchon, P., “Sur les systemes non lineares differentiellement plats.” C. R. Acad. Sci. Paris, t.315, Seriel, pp. 619-624, 1992.
2. Fliess, M., Levine, J., Rouchon, P., “Generalized state variable representation for a simplified crane description”, International Journal of Control, 58(2):277-283,1993.
3. Junkins, J.L. and Kim, Y., “Stability and Control of Tobotic Manipulators ”, AIAA Progress in Astro. And Aero, Vol.161, pp.315-350.
4. Nieuwstadt, M.V., Murray, R.M., “Real Time Trajectory Generation for Differentially Flat Systems”, Submitted International Journal of Robust Nonlinear Control, May 1997.
5. Kato, O., and Sugiura, I., “An Interpretation of Airplane General Motion and Control as Inverse Problem,” Journal of Guidance, Vol. 9, No.2, 1986, pp. 198-204.
6. Kato, O., “Attitude Projection Method for Analyzing Large-Amplitude Maneuvers,” Journal of Guidance, Control, and Dynamics, Vol. 13, No. 1,1990, pp. 22-29.
7. Hess, R. A., Gao, C., and Wang, S.H., “A Generalized Technique for Inverse Simulation Applied to Aircraft Flight Control,” Journal of Guidance, Control, and Dynamics, Vol. 14, No. 5, 1991, pp. 920-926.
8. Gao, C., and Hess, R.A., “Inverse Simulation of Large-Amplitude Aircraft Maneuvers,” Journal of Guidance, Control, and Dynamics, Vol. 16, No. 4, pp. 733-737.
9. Matties, G., Socio, L., and Leonessa, A., “Solution of Aircraft Inverse Problems by Local Optimization,” Journal of Guidance, Control, and Dynamics, Vol. 18, No. 3, 1995, pp. 567-571.
10. Lee, S., Kim, Y., “Solution of the Inverse Simulation Problem by Optimization Technique and it’s Application to Aircraft Nonlinear Large Angle Maneuvers,” AIAA Guidance Navigation and Control Conference, San Diego, CA, July 29­31, 1996.