24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-7.1.2

DESIGN AND EVALUATION OF TACOM CONTROL LOGICS

K. Miyata , T. Udagawa*
Fuji Heavy Industries, Ltd.; *Third Research Center, Technical Research & Development Institute, Japan Defense Agency, Japan

Keywords: UAV, flight control, navigation, launch, target tracking

This paper describes the overview of the control logics of TACOM (Multi-role small UAV, TA-youto K(C)Ogata Mujinki in Japanese) . It is intended to describe key technologies including those related to guidance and control. The evaluation flight test of the TACOM system was completely successful in 2001.

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