‘AeroMech’—Conception of a Generic Stability and Control Methodology

Author:

Chudoba Bernd

Publisher

Springer International Publishing

Reference25 articles.

1. Chudoba, B., “Stability & Control Aerospace Vehicle Design and Test Condition Matrix,” Technical Report EF-039/96, Daimler-Benz Aerospace Airbus, September 1996.

2. Goodrich, K.H., Sliwa, S.M., and Lallman, F.J., “A Closed-Form Trim Solution Yielding Minimum Trim Drag for Airplanes With Multiple Longitudinal-Control Effectors,” NASA TP 2907, NASA Langley Research Center, May 1989.

3. Chudoba, B., “Software Defining Specification for the VORSTAB Aerodynamic Prediction Program,” CoA Report NFP0105, Department of Aerospace Technology, College of Aeronautics, Cranfield University, June 1999.

4. Lan, C.E., “Methods of Analysis in The VORSTAB Code (Version 3.1),” The University of Kansas, May 1993.

5. Lee, H.P., Chang, M., and Kaiser, M.K., “Flight Dynamics and Stability and Control Characteristics of the X-33 Vehicle,” AIAA Paper 98-4410, Guidance, Navigation, and Control Conference and Exhibit, Boston, MA, 10-12 August 1998.

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