Decoupling control design with applications to flight

Journal of Guidance, Control, and Dynamics

Volumn 21, Issue 4, 1998, Pages 647-655

  Snell, Antony ^a,b  

^a UNIVERSITY OF CALIFORNIA   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; BANDWIDTH; CONTROL SYSTEM SYNTHESIS; FEEDBACK; LINEAR CONTROL SYSTEMS; NONLINEAR CONTROL SYSTEMS; SENSORS;

DECOUPLING CONTROL LAWS; DYNAMIC COMPENSATORS;

MULTIVARIABLE CONTROL SYSTEMS;

EID: 0032122073     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4284     Document Type: Article

References (9)

1. Horowitz, I. M., Quantitative Feedback Design Theory (QFT) Vol. 1, QFT Publications, Boulder, CO, 1993, Chap. 14.
2. Snell, A., and Hess, R. A., "Robust Decoupled Flight Control Design with Actuator Saturation," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 3, 1998, pp. 361-367; also AIAA Paper 97-3778, 1997.
3. Enns, D., Bugajski, D., Hendrick, R., and Stein, G., "Dynamic Inversion: An Evolving Methodology for Flight Control Design," International Journal of Control, Vol. 59, No. 1, 1994, pp. 71-91.
4. Lane, S., and Stengel, R. F., "Flight Control Design Using Nonlinear Inverse Dynamics," Automatica, Vol. 24, No. 4, 1988, pp. 471-483.
5. Singh, S. N., and Rugh, W. J., "Decoupling in a Class of Nonlinear Systems by State Variable Feedback," Journal of Dynamic Systems, Measurement and Control, Vol. 94, Dec. 1972, pp. 323-329.
6. Menon, P. K. A., Badgett, M. E., Walker, R. A., and Duke, E. L., "Nonlinear Flight Test Trajectory Controls for Aircraft," Journal of Guidance, Control, and Dynamics, Vol. 10, No. 1, 1987, pp. 67-72.
7. Snell, S. A., Enns, D. F., and Garrard, W. L., "Nonlinear Inversion Flight Control for a Supermaneuverable Aircraft," Journal of Guidance, Control, and Dynamics, Vol. 15, No. 3, 1992, pp. 976-984.
8. Slotine, J. J., and Li, W., Applied Nonlinear Control, Prentice-Hall, Englewood Cliffs, NJ, 1991, Chap. 6.
9. Snell, S. A., "Cancellation Control Law for Lateral-Directional Dynamics of a Supermaneuverable Aircraft," AIAA Paper 93-3775, Aug. 1993.