Inclusion of rotor dynamics in controller design for helicopters

Journal of Aircraft

Volumn 10, Issue 4, 1973, Pages 200-206

  Hall, W E ^a   Bryson, A E ^a  

^a STANFORD UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 85008270776     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.60214     Document Type: Article

References (12)

1. Murphy, R. D. and Narendra, K. S., “Design of Helicopter Stabilization Systems Using Optimal Control Theory,” Journal of Aircraft, Vol. 6, No. 2, March-April 1969, pp. 129-126.
2. Crossley, T. R. and Porter, B., “Synthesis of Helicopter Stabilization Systems Using Modal Control Theory,” Journal of Aircraft, Vol. 9, No. 1, Jan. 1972, pp. 3-8.
3. Kalman, R. E. and Englar, T. S., “A User’s Manual for the Automatic Synthesis Program,” CR-475, June 1966, NASA.
4. Bryson, A. E. and Hall, W. E., “Optimal Control and Filter Synthesis by Eigenvector Decomposition,” SUDAAR 436, Dec. 1971, Stanford Univ., Stanford, Calif.
5. MacFarlane, A. G. J., “An Eigenvector Solution of the Linear Optimal Regulator Problem,” Journal of Electronics and Control, Vol. 14, June 1963, pp. 643-654.
6. Potter, J. E., “Matrix Quadratic Solutions,” SIAM Journal of Applied Mathematics, Vol. 14, No. 3, May 1966, pp. 496-501.
7. Francis, J. G. F., “The QR Transformation,” Computer Journal, Vol. 4, No. 3, Pt. I, Oct. 1961, pp. 265-271; Vol. 4, No. 4, Pt. II, Feb. 1962, pp. 332-345.
8. Hall, W. E., “Computational Methods for the Synthesis of Rotary-Wing VTOL Aircraft Control Systems,” Ph.D. dissertation, Aug. 1971, Stanford Univ., Stanford, Calif.
9. Bryson, A. E., Chasteen, L. H., Hall, W. E., and Mohr, R. L., “Studies of Control and Guidance for Rotary Wing VTOL Vehicles,” SUDAAR419, March 1971, Stanford Univ., Stanford, Calif.
10. Miller, D. P. and Vinje, E. W., “Fixed Based Flight Simulation Studies of VTOL Aircraft Handling Qualities in Hovering and Low-Speed Flight,” TR 67-152, Jan. 1968, Air Force Flight Dynamics Lab., Wright-Patterson Air Force Base, Ohio.
11. Hall, W. E. and Bryson, A. E., “Synthesis of Hover Autopilots for Rotary-Wing VTOL Aircraft,” SUDAAR 446, June 1972, Stanford Univ., Stanford, Calif.
12. Bryson, A. E. and Ho, Y. C., Applied Optimal Control, Xerox-Blaisdell, Lexington, Mass., 1969.