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Synthesis of Aircraft Modal Control Systems having Real or Complex Eigenvalues

Published online by Cambridge University Press:  04 July 2016

T. R. Crossley  and
B. Porter
T. R. Crossley
Affiliation:
Department of Mechanical Engineering, University of Salford
B. Porter
Affiliation:
Department of Mechanical Engineering, University of Salford
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Extract

The theory of modal control is concerned with the design of control loops for systems with governing equations which can be adequately approximated by linear vector-matrix equations of the form

where x is the system state vector, y is the control vector, A is the matrix of the uncontrolled system, and B is the control matrix.

Information

Type
Technical Notes
Information
The Aeronautical Journal , Volume 73 , Issue 698 , February 1969 , pp. 138 - 142
Copyright
Copyright © Royal Aeronautical Society 1969 

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References

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