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Multiparadigm design, validation and verification by simulation in flight control system development

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1 Author(s)
H. H. T. Liu ; Inst. for Aerosp. Studies, Toronto Univ., Ont., Canada

Flight control system development typically involves phases that are often chronological, yet are extensively interrelated and interconnected, where design, validation and verification (DV&V) play a central role. This paper proposes an integrated (DV&V) process aiming at reducing development cycles. A two-way integration approach suggests improvement than the traditional one-way integration approach, in integrating multiparadigm models, heterogeneous simulations, and in including mutual design and validation interactions. The necessity of such an integrated approach is illustrated by a flight control example

Published in:

Computer Aided Control Systems Design, 2004 IEEE International Symposium on

Date of Conference:

4-4 Sept. 2004