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Formation flight technology

T.K. SPEER (Department Engineer)
E.C. MILLS (Aircraft Development Engineer‐Specialist)
J.L. TATE (Electronics Engineer, Lockheed Georgia Co.)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 July 1971

153

Abstract

IN THIS article the evolution of formation flight technology is traced including discussion of the primary characteristics of three specific station keeping system concepts developed by Lockheed‐Georgia. One of the most significant aspects of the overall formation flight problem is that of stability of the formation in a dynamic environment. Detailed simulation studies of the dynamic station keeping geometry have been performed, and the results are presented in the form of fundamental formation flight stability criteria. The extension of present‐day technology to development of formation flight systems for short range aircraft such as helicopters and V/STOL transports is considered briefly.

Citation

SPEER, T.K., MILLS, E.C. and TATE, J.L. (1971), "Formation flight technology", Aircraft Engineering and Aerospace Technology, Vol. 43 No. 7, pp. 4-8. https://doi.org/10.1108/eb034785

Publisher

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MCB UP Ltd

Copyright © 1971, MCB UP Limited

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