Stochastic optimal control of flexible aircraft taxiing at constant or variable velocity

Author:

Ming Zhang,Hong Nie,Rupeng Zhu

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Applied Mathematics,Mechanical Engineering,Ocean Engineering,Aerospace Engineering,Control and Systems Engineering

Reference20 articles.

1. McGehee, J.R., Carden, H.D.: Improved aircraft dynamic response and fatigue life during ground operations using an active control landing gear system. In: AlAA Aircraft Systems and Technology Conference, Los Angeles, CA, pp. 78–1499, August 21–23, 1978

2. Irving, R., Ralph, E.: An electronic control for an electrohydraulic active control aircraft landing gear. NASA CR-3113 (1979)

3. Irving, R., Ralph, E.: An electronic control for an electrohydraulic active control landing gear for the f-4 aircraft. NASA CR-3552 (1982)

4. Freymann, R.: Actively damped landing gear system, landing gear design loads. AGARD CP-484 (1990)

5. Daniels, N.J.: A method for landing gear modeling and simulation with experimental validation. NASA CR-201601 (1996)

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