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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
Affiliation:
Department of Mechanical Engineering, University of Salford
B. Porter
Affiliation:
Department of Mechanical Engineering, University of Salford

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
Copyright
Copyright © Royal Aeronautical Society 1969 

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