您要查找的是不是：
- Subsystems of flight control system II. 飛行控制系統的分系統2。
- 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。
- 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。
- 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)。
- The flight control system can record 8 different flight paths and separate paths can be grouped to build new path. 飛行控制系統可記錄8個(gè)不同的飛行路徑動(dòng)作，且可以將單個(gè)飛行路徑組合起來(lái)形成新的飛行路徑。
- Multi-loop feedback control was employed for underactuated flight control system of unmanned helicopter. 摘要針對無(wú)人直升機欠驅動(dòng)特性，采用多回路反饋方法設計飛行控制系統。
- AUTOMATIC FLIGHT CONTROL SYSTEM, A system composed of all necessary subsystems needed to guide the flight of an airplane. 自動(dòng)飛行控制系統,由所有能引導飛機飛行的子系統所組成的一個(gè)系統。
- Because these wind loads are a major structural consideration, they greatly influence the design of the flight control system. 因為這些風(fēng)載荷是結構上主要的考慮因素，它們很大地影響著(zhù)飛行控制系統的設計。
- A new inner/outer loop structure is proposed, and its application to the design of helicopter flight control system is described. 提出了一種新型的內／外回路控制結構，系統地闡述了此結構在直升機控制系統中的應用。
- 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。
- The distributed flight control system is designed by using the ACE ORB (TAO) middleware and its event service mechanism. 摘要利用中間件TAO及其事件服務(wù)機制，設計了分布式飛行控制系統。
- The part two discusses some issues that relate to the design and construction of the redundant Digital Flight Control System(DFCS). 第二部分討論了多余度數字式飛行控制系統設計和實(shí)現時(shí)的幾個(gè)問(wèn)題 。
- The simulation results show that designed flight control system can complete required maneuvering flight and possesses excellent tracking performance. 仿真結果表明:采用文中提出的設計方案,所設計的飛行控制系統能夠完成要求的機動(dòng)飛行動(dòng)作并且具有優(yōu)良的跟蹤性能。
- He has conducted the design work of flight control system of “M16” helicopter and automatic pilot system of the coaxial unmanned helicopter. 主持設計了“M16”型直升機的操縱系統和共軸式無(wú)人駕駛直升機的自動(dòng)駕駛儀系統。
