Eigenstructure assignment with gain suppression using eigenvalue andeigenvector derivatives

Journal of Guidance, Control, and Dynamics

Volumn 13, Issue 6, 1990, Pages 1008-1013

  Sobel, Kenneth M ^a   Yu, Wangling ^a   Lallman, Frederick J ^b  

^a CITY COLLEGE OF NEW YORK   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT, MILITARY--CONTROL; CONTROL SYSTEMS; DYNAMICS;

EIGENVECTORS; FEEDBACK;

MATHEMATICAL TECHNIQUES;

EID: 0025510407     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.20573     Document Type: Article

References (8)

1. Andry, A. N., Shapiro, E. Y., and Chung, J. C., “Eigenstructure Assignment for Linear Systems,” IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-19, Sept. 1983, pp. 711-729.
2. Calvo-Ramon, J. R., “Eigenstructure Assignment by Output Feedback and Residue Analysis,” IEEE Transactions on Automatic Control, Vol. AC-31, No. 3, 1986, pp. 247-249.
3. Srinathkumar, S., “Eigenvalue/Eigenvector Assignment Using Output Feedback,” IEEE Transactions on Automatic Control, Vol. AC-23, No. 1, 1978, pp. 79-81.
4. “Flying Qualities of Piloted Airplanes,” U.S. Military Specification, MIL-F-8785C, Nov. 1980.
5. Lim, K. B., Junkins, J. L., and Wang, B. P., “Re-Examination of Eigenvector Derivatives,” Journal of Guidance, Control, and Dynamics, Vol. 10, No. 6, 1987, pp. 581-587.
6. Press, W. H., Flannery, B. P., Teukolsky, S. A., and Vetterling, W. T., Numerical Recipes: The Art of Scientific Computing, Cambridge Univ. Press, New York, 1987.
7. Moler, C., Little, J., and Bangert, S., PC-MATLAB for MS-DOS Personal Computers, The Mathworks Inc., Sherborn, MA, Version 3.2-PC, June 1987.
8. Lehtomaki, N. A., Sandell, N. R., Jr., and Äthans, M., “Robustness Results in Linear Quadratic Based Multivariable Control Designs,” IEEE Transactions on Automatic Control, Vol. AC-26, No. 1, 1981, pp. 75-92.