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- Flight Test Activity 試飛活動(dòng)
- Participate in the flight test procedures improvement. 參與試飛程序的完善。
- Research of JL8 aircraft stall and spin flight test is described in this paper. 敘述了JL8飛機失速尾旋試飛狀態(tài)、試飛方法和試飛結果。
- Any flight test and wind tunnel correlation always suffers from a great number of unknowns. 在對飛行試驗與風(fēng)洞試驗進(jìn)行比較時(shí)總有大量的未知數。
- This marks the second time the NLOS-LS CLU was used in a flight test of the PAM missile. NLOS-LS為指揮官提供即時(shí)、精確響應的火力，打擊移動(dòng)和靜止的陸地、海上目標。
- The flight test monitor and command system is main part of flight test engineering. 試飛監控與指揮系統是飛行試驗工程中的重要組成部分。
- In addition, preliminary proof for the half system flight test program of SITAN algorithm was discussed. 此外還對SITAN系統半 系統試飛方案作了初步的論證工作。
- Describe the basic progression of the first flight tests. 請描述一下首飛測試的基本過(guò)程。
- The poesend problems in evaluation antiship missile flight test are pcinted out. 指出現行反艦導彈飛行試驗結果評定的命中域標準存在的問(wèn)題。
- Due to the mission at the Air Force Flight Test Center, it operates a great variety of aircraft. 由于在空軍班機測試中心的任務(wù)，它操作飛機的一個(gè)很棒的多樣性。
- Another strong impression is that the airplane wants to fly a lot faster than we are allowed to fly at this point in the flight test program. 另外一個(gè)深刻印象就是這架飛機總是要比我們在當前試飛進(jìn)度所允許的飛行速度飛的快一點(diǎn)。
- Wang, Z., Li, J., Lan, C. E. and Brandon, J. M., "Estimation of Unsteady Aerodynamic Models from Flight Test Data", AIAA Paper 2001-4017, August 2001. 飛機氣動(dòng)力建模講習會(huì ),地點(diǎn)：中華航空公司(臺北松山機場(chǎng))，主辦單位：國立成功大學(xué)航空太空工程系，2002年12月。
- Flight test vehicles require a certain degree of wiring and installation modification to accommodate flight test equipment. 飛行試驗機需要一定程度的配線(xiàn)和安裝改動(dòng)來(lái)適應飛行測試設備。
- In the paper the correlations of the wind tun-nel results with flight test restults,and pilot's evaluation to the flying qualities are pre-sented. 文中還給出了風(fēng)洞實(shí)驗和飛行試驗的相關(guān)性以及飛行員對飛行品質(zhì)的評估。
- An analysis of flight test results was conducted to explain the effects of winglets on aerodynamic load, control-stability and performances. 本文對翼尖小翼的飛行試驗結果進(jìn)行了分析,試圖說(shuō)明它對飛機的氣動(dòng)載荷、操穩特性及飛行性能的影響。
- The examinee examination mold was mainly used for dynamic testing activity, examination time locking, automatic system grading and out-bursting problem solution. 考生考試模塊主要實(shí)現動(dòng)態(tài)隨機出題、考試時(shí)間鎖定、系統自動(dòng)判卷和突發(fā)問(wèn)題應對等功能。
- A kind of aircraft radome checked by this method has undergone flight tests. 該方法驗證的天線(xiàn)罩防冰裝置已經(jīng)經(jīng)歷了飛行的考驗。
- The wind tunnel and flight test investigations show that the new conception of configuration of MAV is feasible,and compared. 在此基礎上,進(jìn)行了柔性-剛性混合翼微型飛行器試驗原理樣機的飛行試驗驗證。
- Then the paper studies the application of LMI filtering method in the flight test data processing.A new LMI robust filter is provided. 并以飛行試驗數據濾波處理為例，研究了LMI濾波技術(shù)的應用，設計出了基于LMI的魯棒濾波器。
- To delivery, and as a consequence puts test activities unnecessarily on the critical path of the project. 交付而完成測試準備,并且作為將不必要的測試活動(dòng)放在項目的關(guān)鍵路徑上的結果。
