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- Abstract: A type of pilotless target aircraft flight control system is introduced.The function and basic compose and autopilot control regular and engine control principle and recovery control scheme of the flight control system are discussed. 文摘:介紹了無(wú)人駕駛靶機的飛行控制系統，詳細討論了系統的功能、基本組成、自動(dòng)駕駛儀控制規律、發(fā)動(dòng)機控制原理、回收控制方案及系統軟件設計等。
- The Design of the Pilotless Target Aircraft Flight Control System 無(wú)人駕駛靶機飛行控制系統設計
- Subsystems of flight control system II. 飛行控制系統的分系統2。
- Another aerodynamic improvement is the Digital Flight Control System, which improves the aircraft's reliability and reduces airframe weight. 另一個(gè)改進(jìn)是氣動(dòng)數字飛行控制系統，提高了飛機的可靠性和降低了機身重量。
- A technique which used to design the flight control system for a highly maneuverable aircraft was described, and the related simulation was finished. 摘要對超機動(dòng)飛機在大迎角機動(dòng)下的控制律進(jìn)行設計，并完成相關(guān)仿真驗證。
- Using this method, the flight control law which suits to the vectored aircraft flight in post-stall domain is designed in this paper.3. 運用這種方法對推力矢量飛機進(jìn)行了適用于過(guò)失速機動(dòng)的非線(xiàn)性飛行控制系統設計。
- Simulation results show that the EHA can meet modern aircraft's requirements to the actuate system, and it can be used widely in the future PBW flight control system. 結果表明,EHA的性能能夠滿(mǎn)足現代飛機對作動(dòng)系統的要求,在未來(lái)功率電傳(PBW)的飛控系統中具有很好的應用前景。
- To optimize the parameters of the aircraft s flight control system(FCS),a reference model method based on the niche genetic algorithm(NGA)is proposed in this paper. 針對飛行控制系統控制器參數優(yōu)化問(wèn)題,提出了一種基于小生境遺傳算法的模型參考優(yōu)化整定策略,并將此策略應用于某型飛機的橫側向飛行控制系統的參數優(yōu)化中。
- The pilot controls the aircraft is supplemented by an Automatic Flight Control System(AFCS) and a Thrust/Power Management System. 該飛機控制系統結合旋翼控制和固定翼控制,通過(guò)自動(dòng)控制系統和推力管理系統來(lái)輔助飛行員對飛機的控制。
- The design of the flight control system with the vectored thrust is discussed. 對帶推力矢量飛機的飛控設計問(wèn)題進(jìn)行了研究。
- And during this case, flight control system (FCS) plays a more important role . 在上述改進(jìn)的基礎上,飛行控制系統起到關(guān)鍵性的作用。
- Missile rudders are executive bodies of missile flight control system. 舵機測試系統是導彈生產(chǎn)線(xiàn)上的重要設備。
- flight control system of aircraft 飛機飛行控制系統
- ALTITUDE ACQUIRE, A digital flight control system mode to transition from climb (or descend) to level flight. 高度截獲,一種數字式飛行操縱系統,從爬升(或下降)改平的模式。
- That defect could cause solders to crack and the flight control system to fail, Ernst explains. 他拒絕提供細節，他的觀(guān)點(diǎn)是，假零件肯定會(huì )導致嚴重事故。
- A new approach based on LPV model to design large envelope flight control system is presented. 介紹一種基于線(xiàn)性參變模型(LPV)設計大包線(xiàn)飛行控制器的新方法。
- Abstract: The design of the flight control system with the vectored thrust is discussed. 文摘:對帶推力矢量飛機的飛控設計問(wèn)題進(jìn)行了研究。
- Abstract： The design of the flight control system with the vectored thrust is discussed. 摘 要： 對帶推力矢量飛機的飛控設計問(wèn)題進(jìn)行了研究。
- This paper described the primary impact factors of design of an automatic flight control system (AFCS) for commercial aircraft, such as the impact of aircraft configuration,the sensors onboard performance primary flight handling system. 本文論述了在飛機自動(dòng)飛行控制系統中,影響設計的主要因素,如飛機構形的影響,機上傳感器的影響以及主操縱系統結構的影響。 并討論了多輸入多輸出問(wèn)題;
- The research emphasis of flight control system of UAH is to determine the flight states of UAH by use of measured data. 利用有限的測量數據來(lái)確定無(wú)人直升機的飛行狀態(tài)變量是無(wú)人直升機飛行控制系統研究的熱點(diǎn)。
