06-國外無人直升機及其關鍵技術發(fā)展-資料下載頁
2025-06-25 05:07本頁面
【正文】 為無人直升機研制的機載設備、系統(tǒng)及武器還非常少，可以說幾乎沒有，不過，可以預計，在不久的將來，這類研究工作將開始受到人們的高度關注，美國國家航空航天局陸軍研究實驗室著手專門為無人直升機開發(fā)一種可以燃燒重油的“擺盤”發(fā)動機就是一個很好的例證。6） 除了技術因素以外，無人直升機關鍵技術的突破還是一項長期的、需要大投入的研究活動。參 考 文 獻[1] , Possible rotorcraft configurations for unmanned application, RPVS [2] .BassetJ.Deslous, Performances parisons of differect rotary wing UAV configurations, 31ERF, 2005[3] , , Mathemeatical Modeling and Experimental Identification of a Model Helicopter, AIAA984357[4] Bourhance Kadmiry, Fuzzy Control for an Unmanned Helicopter, ISSN 02807971[5] Bernad Mettler, Mark , Takeo Kanade, System Identification of Small—Size Unmanned Helicopter Dynamics, 55th AHS International Annual Forum Proceedings, May, 1999[6] Bernad Mettler, Mark , Takeo Kanade, System Identification of Small—Size Unmanned Rotorcraft for Flight Control Design, 58th AHS International Annual Forum Proceedings, May, 2002[7] Jason D. Colbourne, Cal Poly Foundation, System Identification and Control System Design for the BURRO Autonomous UAV, 56th AHS International Annual Forum Proceedings, May, 2000[8] . Mcdade, . Spencer, Modular Electronics for Tilt Rotor UAV Payloads, 48th AHS International Annual Forum Proceedings, 199239 / 7
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