An interpretation of airplane general motion and contol as inverse problem

Journal of Guidance, Control, and Dynamics

Volumn 9, Issue 2, 1986, Pages 198-204

  Kato, Osamu ^a   Sugiura, Ichiro ^a  

^a NAGOYA UNIVERSITY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

EQUATIONS OF MOTION;

ATTITUDE ANGLES; FORCE EQUATIONS; INVERSE PROBLEM; PATH ANGLES;

AIRCRAFT;

EID: 0022679659     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.20090     Document Type: Article

References (10)

1. Jones, R.T., “A Simplified Application of the Method of Operators to the Calculation of Disturbed Motions of an Airplane,” NACA TR 560, 1936, pp. 313-325.
2. Weick, F.E. and Jones, R.T., “The Effect of Lateral Controls in Producing Motion of an Airplane as Computed from Wind-Tunnel Data,” NACA TR 570, 1936, pp. 465-490.
3. Etkin B., Dynamics of Flight, John Wiley & Sons, New York, 1959.
4. Meyer, G. and Cicolani, L., “A Formal Structure for Advanced Automatic Flight-Control Systems,” NASA TN D-7940, 1975.
5. Meyer, G. and Cicolani, L., “Application of Nonlinear Systems Inverses to Automatic Flight Control Design—System Concepts and Flight Evaluations,” Theory and Applications of Optimal Control in Aerospace Systems, edited by I.P. Kant, AGARDograph 251, 1981.
6. Ehrend W.R. Jr., “Pilot Control through the TAFCOS Automatic Flight Control System,” NASA TM-81152, 1979.
7. Korenev, G.V., The Mechanics of Guided Bodies, London Iliffe Books Ltd., 1967.
8. Perkins, C.D. and Hage, R.E., Airplane Performance Stability and Control, John Wiley & Sons, New York, 1949, pp. 12-13, 452-458.
9. Etkin, B., Dynamics of Atmospheric Flight, John Wiley & Sons, New York, 1972, p. 114.
10. McRuer D., Ashikenas I., and Graham D., Aircraft Dynamics and Automatic Control, Princeton University Press, 1973, pp. 701-704.