flight order 中文意思是什麼
flight order
解釋
飛行命令-
A pure software solution is given in order to gather more tracking data. the reason of the zenith - blind - zone forming is analyzed detailedly. the conclusion is that the extent of the zenith blind zone was restricted by three parameters : maximum azimuth angular velocity of tracking mount, flight level and airspeed of the target
本文依據不改變系統硬體結構的研究思路，提出一個基於目標軌跡預測技術的解決過天頂跟蹤的方案構想，給出具體實施步驟，預計可使系統單站單圈次跟蹤採集到的有效數據總量提高約一倍。 -
In order to learn flight, he developed a friendship with the drillmaster
為了學習飛行，他和教官交上了朋友。 -
As part of the airtransport agency, our company gets freight transportation order from the customer and decide flight route ; and then divide the goods and choose the flight according to the specific airport
作為航空貨代業務的一部分，我公司從客戶取得貨運訂單，決定飛行路線，根據特定機場分撥點拼箱集運貨物，以及選擇航班。 -
In order to make the terminal airspace moderated and consisted, and acquire the biggest capacity of airport, we must consider the influencing factors as many as possible, it is our final target to plan the airspace in beijing terminal unify. with the conditions that the current operation modes of parallel runway, approach and departure procedures and terminal airspace in beijing international airport, this article has analyzed the reasons of airspace congestion. this article also applies the theory of instrument flight procedure and utilizes the current facilities in beijing international airport. the design of flight procedures combining rnav procedures with instrument approach procedures may be accepted on some routes. it make the approach and departure procedure more effective, and increase the capacity of the airport more or less ; secondly, this article contrast the capacities of parallel runway in different methods under radar control, and make the conclusion that the parallel runway in dependent operation modes has the biggest capacity
本文從目前首都機場平行跑道的運行方式、進離場程序、終端區空域的現狀入手，剖析了造成空域緊張的原因，應用儀表飛行程序設計的思想和原則，利用首都機場終端區現有的設施，某些航線可採用區域導航（ rnav ）程序與儀表進近程序相結合的飛行程序設計，優化了目前首都機場的進離場程序，在一定程度上增加了機場容量；其次，研究了雷達管制條件下平行跑道不同運行方式的容量對比，得出平行跑道獨立運行的容量最大，然後以這種這種運行方式，為首都機場設計出了平行跑道獨立運行的飛行程序；最後，分析北京終端區各機場空域對首都機場飛行程序安全、有效運行的制約因素，研究設計出了北京終端區規劃方案及規劃后的飛行程序和飛行方法，以達到增大機場的容量，適應未來航班量增加的需求。 -
Article 207 where a civil aircraft, in violation of the provisions of article 74 of this law, conducts flight activities without the approval of the air traffic control unit, the competent civil aviation authority under the state council shall order it to stop flying, and impose a fine on the owner or lessee of the civil aircraft of not less than 10, 000 yuan but not more than 100, 000 yuan ; and punish the pilot - in - command of the civil aircraft by warning or by withholding his licence for a period of one to six months, or under aggravating circumstances, punish him by cancelling his licence
第二百零七條違反本法第七十四條的規定，民用航空器未經空中交通管制單位許可進行飛行活動的，由國務院民用航空主管部門責令停止飛行，對該民用航空器所有人或者承租人處以一萬元以上十萬元以下的罰款；對該民用航空器的機長給予警告或者弔扣執照一個月至六個月的處罰，情節較重的，可以給予吊銷執照的處罰。 -
Spinning flight of ballistic missile in boost phase is a new idea in order to penetrate laser ’ s interception. spinning missiles may be unstable due to dynamic and control interactions
彈道導彈主動段自旋飛行是一種新的構想，旨在對抗激光武器攔截，實現主動段突防。 -
In order to study the flight characteristics and control rules in taking off and landing period better to promote flight safety of uav in this stage, we started the study of take off and landing simulation system research of uav based on a certain type of uav
為更好地研究無人機在起飛、著陸階段的飛行特性，控制規律，以保證無人機在這一階段的飛行安全，我們以某型無人機為對象進行無人機的起飛、著陸模擬系統研究。 -
In the range of flight mach number mo = 3 ~ 7, in order to take the advantage of ramjet and scramjet, a fix - shaped dual - mode scramjet, in which both subsonic and supersonic combustion can be obtained, is used for hypersonic vehicle
在飛行馬赫數m _ = 3 - 7的范圍內，為充分發揮沖壓發動機的性能優勢，高超聲速飛行器採用了既能在亞聲速燃燒模態，又能在超聲速燃燒模態下工作的固定幾何形狀的雙模態沖壓發動機。 -
According to purpose of the towed flight, a new trajectory consisting of taking off, climbing phase, level flight phase is presented with. trajectory pitch angle of the towing plane is optimized. according to the flight law of the towing plane, the fin deflection angle and amplification coefficient of particle - system trajectory of carrier rocket are designed, in order to realizing flight steadily of the carrier rocker
根據牽引飛行的目的，對載機應用了「起飛?爬升?平飛」的變軌道飛行方案，同時對載機軌道的傾角、傾角變化規律進行優選設計；再根據載機的飛行規律，對運載器質點系軌道的舵偏規律及其放大系數進行了設計計算，實現運載器穩定牽引飛行。 -
Commit other acts endangering flight safety and disturbing the order in aircraft
五）危及飛行安全和擾亂航空器內秩序的其他行為。 -
It has been maked for immediate and statistical analysis that the calculation about the work order parameter of the base - bleed - rocket is calculated in the taguchi method, its influencing trend is bring out in the open, the theoretical base is settled for confirming the greatest combination about the work order parameter of the base - bleed - rocket. the multi - objectile optimal design model is established that the indexes have been taked into account first and synthetically, such as physical parameter range lethality power strength and flight stability and so on, the program is compiled and the example is calculated. the true worth of the theoretical work in this paper is validated by flight experimentation of 130mm hybrid base - bleed - rocket extended - range principium projectile
本文進行了底排?火箭復合增程彈工作時序參數正交試驗設計的直觀分析與方差分析，揭示了每個參數對射程計算的影響趨勢，為進一步確定底排?火箭工作時序參數值的最佳匹配組合奠定了理論基礎；建立了底排?火箭復合增程彈多目標優化設計模型，該模型首次綜合考慮了底排?火箭復合增程彈的結構特徵參量、結構強度性能、飛行穩定性、威力性能和射程指標，編制了相應的分析程序，進行了算例計算；完成了130mm底排?火箭復合增程原理樣彈的結構設計與飛行試驗，其試驗結果驗證了本文理論研究工作的實際應用價值。 -
In order to improve the resolution power, the energy method need increase ion total energy, while, the choice of the right gas pressure, the right flight length and increase total energy are effective to improvement of resolution for gf - tof method
增加對同量異位素的分辨能力，對e - e探測方法就要增加離子能量，而gf - tof方法除了增加離子能量外，合理的選擇飛行路徑的長度也能提高分辨能力。 -
In order to determination the thrust, the thrust definition and many control parameters are analyzed discussed, which mass flow rate and flight altitude are involved. it is difficult to measure the flight thrust of solid rocket ramjet directly
通過討論高空飛行推力與地面可測試參數的關系，得到了固體火箭沖壓發動機高空飛行狀態下推力折算方法，並開發相應的計算程序。 -
" in order to ensure flight safety the cad has been active in promoting new safety requirements relating to the avoidance of fatigue in aircrews and to this end, the flight time limitations working group ( ftlwg ) was established in 1997
發言人說：為了保障飛行安全，民航處一向積極推廣避免飛行員過勞的新規定。飛行時間限制工作組遂於一九九七年成立，檢討有關計劃的現行條文，並且因應超長航距運作而訂立所需的要求。 -
Use energy - based control method to achieve the entry flight control of reusable launch vehicle. the basic concept is to take the energy as primary control variables, reduce the order of the system and design a tracking law to follow a three - dimensional entry trajectory
本文採用基於能量的控制方法實現對航天器再入軌跡的控制，將能量作為獨立參量，從而降低系統的階數，利用線性反饋的方法設計一個跟蹤三維再入軌跡的控制律。 -
Fly to the school directly : if want to reach the school directly, it is in order to choose the route with least dot of a favourable turn normally most zhui, will can reduce the time of the flight, 2 come also the machine rate that bring down baggage loses
直接飛抵學校：假如想直接到達學校，通常以選擇轉機點最少的航線為最隹，一來可以減少飛行的時間，二來亦減低行李遺失的機率。 -
But the variation of its aerodynamic forces will induce flapping motion and produce the cyclic pitch on the main rotor blades by the bell mixing mechanism. in order to study the effect of bell - hiller stabilizer bar on helicopter stability and control, this paper first analyze the function and the principles, give the flapping equation and a flight dynamic model with bell - hiller stabilizer bar. and then works over the stability and control of uav r - 50 in hover and cruise condition, and analyzed the influence from parameters of the bar to it
為了深入研究希勒伺服旋翼對直升機穩定性和操縱性的影響，本文首先分析了希勒伺服旋翼的功能和工作原理，推導了伺服旋翼的揮舞運動方程，建立了帶有希勒伺服旋翼直升機的飛行動力學模型，然後以yamahar - 50無人直升機為例，分析該直升機在懸停和前飛時的平衡、穩定性和操縱性，在此基礎上進一步研究希勒伺服旋翼設計參數變化對直升機穩定性和操縱性的影響。 -
In order to smooth the air traffic flow, the delay time and new schedules of flight are obtained through solving the numerical examples
然後對模型進行了具體的數例求解，得到航班的延遲時間和新的航班時刻，達到了平滑交通流量的目的。 -
After achieving the australian commercial pilot licence, the cadets would need to undergo further flight and theory training with bae systems in order to pass the hong kong flight tests and ground examinations for the purpose of converting their australian licence into hk cplir
學員在取得澳洲商用飛機駕駛執照后，需要在英國宇航航空訓練學校接受進一步飛行和理論訓練，以期通過香港飛行測試和地面考核，方可把澳洲執照轉換為具備儀表飛行等級的香港商用飛機駕駛執照。 -
Air navigation flight prohibition order commencement notice 2005
飛航飛行禁制令2005年生效日期公告
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