【正文】
為無人直升機(jī)研制的機(jī)載設(shè)備、系統(tǒng)及武器還非常少,可以說幾乎沒有,不過,可以預(yù)計(jì),在不久的將來,這類研究工作將開始受到人們的高度關(guān)注,美國國家航空航天局陸軍研究實(shí)驗(yàn)室著手專門為無人直升機(jī)開發(fā)一種可以燃燒重油的“擺盤”發(fā)動(dòng)機(jī)就是一個(gè)很好的例證。6) 除了技術(shù)因素以外,無人直升機(jī)關(guān)鍵技術(shù)的突破還是一項(xiàng)長期的、需要大投入的研究活動(dòng)。參 考 文 獻(xiàn)[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