Piloted simulation tools for aircraft departure analysis

Author:

Patel Yoge1,Littleboy Darren1

Affiliation:

1. Defence Evaluation and Research Agency, Bedford MK41 6AE, UK

Publisher

The Royal Society

Subject

General Physics and Astronomy,General Engineering,General Mathematics

Reference15 articles.

1. Adams Jr W. M. 1972 Analytical prediction of airplane equilibrium spin characteristics. NASA Technical Note NASA-TN-D-6926 Langley Research Centre.

2. Gibson L. Nichols N. K. & Littleboy D. M. 1997 Closed loop design for a simple non-linear aircraft model using eigenstructure assignment. AIAA-97-3779 AIAA AFM Conference New Orleans.

3. Goman M. G. & Khramtsovsky A. V. 1995 A review of bifurcation theory methods in nonlinear flight dynamics problems: application to HIRM high angle of attack dynamics. Contract Report produced by TsAGI Moscow for DERA Bedford.

4. Goman M. G. Khramtsovsky A. V. & Usoltsev S. 1995 High incidence aerodynamics model for hypothetical aircraft. Contract Report 15/5 produced by TsAGI Moscow for DERA Bedford.

5. Goman M. Fedulova E. & Khramtsovsky A. 1996 Maximum stability region design for unstable aircraft with control constraints. AIAA-96-3910 AIAA AFM Conference San Diego.

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5. Basics of MAV Flight Control;Encyclopedia of Aerospace Engineering;2010-12-15

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