Compatibility Aspects of Active Control Technologies with Aircraft Structure Design

Author:

Becker J.,Weiss F.,Sensburg O.

Publisher

Springer Netherlands

Reference5 articles.

1. Collmann, K.D. and Sensburg, O., “Impact of a command and stability augmentation system on gust response of a combat aircraft”, 44th Meeting of the SMP of AGARD, Lisboa, April, 1977.

2. Zimmermann, H. and Sensburg, O., “Impact of active control technology on structures”, Presentation at the 37th Annual Conference of the Society of Allied Weight Engineers (SAWE), SAWE-Paper No. 1242, Index Category No. 22, May, 1978.

3. Sensburg, O., Becker, J. and Honlinger, H., “Active control of flutter and vibration of an aircraft”, Proceedings of the International IUTAM Symposium, June, 1979.

4. Sensburg, O., Becker, J., Lusebrink, H. and Weiss, F., “Gust load alleviation on Airbus A300”, Presentation at the 13th Congress of the International Council of the Aeronautical Sciences (ICAS), August, 1982.

5. Becker, J., Weiss, F., Cavatorta, E. and Caldarelli, G., “Gust alleviation on a transport airplane”, AGARD-Symposium on ‘Unsteady Aerodynamics’, Fundamentals and applications to aircraft dynamics, May, 1985.

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