flight function 中文意思是什麼

flight function 解釋
飛行操縱動作
  • flight : n 1 飛行,飛翔;(鷹對獵物的)追趕。2 (候鳥等的)遷徙;飛行的一群。3 (光陰)飛逝。4 (思想等的...
  • function : n 1 功能,官能,機能,作用。2 〈常 pl 〉職務,職責。3 慶祝儀式;(盛大的)集會,宴會。4 【數學】...
  1. Matlab / stateflow has a power function of logical management. flight manage system can be edited by stateflow with complex logical management. through the system uav can fly independently or fly by remote control. a power window to display the number and flight course is edited by matlab / gui, through the window flight control parameters and flight state can be adjusted

    利用stateflow強大的邏輯和圖形化編程功能模擬了無人機的飛行管理器,實現了自主飛行和遙控飛行的功能;利用gui用戶圖形界面建立了功能強大的人機界面,對simulink中的模擬數據進行顯示。
  2. The method of wing shape optimization of space shutlle has been developed with penalty function approach in which the objective function is the mass of the wing and the constraints are the hypersonic re - entry flight cross range, lift / drag ratio, and subsonic flight lift / drag ratio, the margin of the longitudial static stability and the magnitude of the horizontal landing speed etc

    摘要介紹了在滿足高超音速再入橫向機動航程,高超音速再入飛行時的升阻比,亞音速進場飛行時的升阻比,縱向靜穩定性裕度和水平著陸速度等飛行性能設計要求下,用罰函數法尋求使航天飛機機翼質量為最小的外形優化方法並給出了算例。
  3. A mathematical model reflecting the tilt rotor unsteady and nonlinear aerodynamic characteristics in the longitudinal channel is presented in the paper. in the full flight envelope, the rotor thrust continues tilting and the aerodynamic forces of each component change as a function of airspeed and nacelle angle

    在整個飛行包線內,旋翼的推力矢量方向不斷變化,飛機各部件的氣動力隨發動機短艙傾角和空速的變化而變化,因而飛機的飛行動力學有很強的非定常、非線性特性。
  4. When solving the tna problem based on fleet balance application, a flight pairing network model is build, by which the primary problem transferred to a directed path decomposition problem to minimize target function, and a simulated annealing algorithm is constructed

    在解決使飛機均衡使用的飛機排班問題時,本文利用航班節的網路模型將原問題轉化為一個使目標函數最小的航班節編組問題,在此基礎上構造了一個模擬退火演算法。
  5. The final software has four function levels and can run in three different modes : flight control, test end parameters tuning

    最終設計的飛行控制軟體具有4個功能層次,能夠在飛控、測試和調參3種模式下運行。
  6. With the development of space exploration projects, the atrophy and decreased function in antigravity skeletal muscles are one of major problems that need to be solved for the prolonged space flight. to understand the features of decreased contractile function and increased fatigability in unloaded hindlimb skeletal muscles will help to develop effective countermeasures during space flight, and contribute to the prevention and treatment of skeletal muscle atrophy in long - term bed - rest patients

    隨著載人航天活動的發展,航天飛行時間越來越長,抗重力肌廢用性萎縮引起的強直收縮疲勞性增加,使航天員運動易疲勞的感覺更加明顯,限制了飛行時間和工作效率,在應急逃生時肌肉發生損傷的可能性增大,且影響返回地面重力環境后的再適應能力。
  7. Thirdly, we discussed how to define the software architecture based on the structure and function of flight information subsystem. the software architecture defines the framework of the design and analysis process. the use of client - server architecture makes the flight information subsystem high extendibility

    在分析了飛行情報子系統的基本功能和典型用例基礎上,確定了飛行情報子系統的客戶服務器模式的軟體體系結構,從而為飛行情報子系統的詳細分析設計確定了總體框架,也保證了飛行情報子系統的可擴展性。
  8. Based on the firsthand observation information obtained from air observation, this paper gived a second extrapolation to aircraft possible flight path and made checks on targets relativity by the method of utility function overall evaluation, accomplished the data fusion of targets information, and resolved the problem of relating of air observation information fusion and flight path extrapolation

    摘要在得到對空觀察哨直接觀測信息的基礎上,對目標可能航向進行二次外推,並利用效用函數綜合評估法對目標相關性進行檢驗,完成對目標信息的融合,解決了觀察哨情報數據關聯和航跡外推問題。
  9. The main function of orbit calculation is to simulate the flight procedure of spacecraft, before that, the dynamics model of orbit must be established

    軌道計算主要用來模擬飛行器的飛行過程,前提是建立動力學模型。由於空間問題的復雜性,造成了動力學模型的多樣性。
  10. 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。
  11. Architectural language is adopted to express the special function of the ap - mcsta headquarters building for aviation and space flight

    摘要用建築的語言表述亞太空間合作組織總部大廈航空、航天、航宇的內在特質。
  12. A flight trajectory math model of an assumed cruise aircraft is built according to a simple blue print of the flight control system, with the foundation of a particular analysis of its kinematics and dynamics. a linear light - disturbed minor - cycled movement model and the transform function models are got through some simplifications

    本文以某個虛構的巡航式飛行器的飛行控制系統為研究對象,首先討論了一個簡單的總體方案,然後根據此方案,在詳細分析此飛行器運動學與動力學的基礎上,建立了飛行器飛行模擬數學模型,並在允許的條件下進行簡化得出了此飛行器線性化小擾動短周期運動模型與傳遞函數模擬模型。
  13. The function requirements of commercial camera unmanned aerial vehicle ( uav ) flight controller software are given

    摘要介紹了民用攝像無人機飛行控制器軟體的功能需求。
  14. Firstly, the task, structure, technology and function of the existing dispatch system were introduced, whose key technology is based on the tdm and time division switch like pstn. further, the developing direction of pstn is based on ip, the pocked switch system and network, and also the dispatch system of the manned space flight launch base will transmit multimedia information on ip

    首先,介紹了現有調度系統的任務、結構、技術和功能,可以看出,其技術核心是時分多路復用和時分交換技術,現在公用交換電話網( pstn )正向基於ip的包交換系統和網路發展,載人航天發射場調度系統也將利用ip網路技術傳輸多媒體指揮信息。
  15. 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、自動駕駛儀控制規律、發動機控制原理、回收控制方案及系統軟體設計等。
  16. Using opengl and c + + builder6. 0, we developed a flight simulation software - lightdream1. 0. this software effectively implemented the real time flight monitoring function, flight simulation, path planning and displaying functions which satisfied the requirement of flight control system simulation of unmanned helicopter

    最後,採用borlandc + + builder6 . 0開發平臺和opengl圖形開發庫,開發完成了一套飛行模擬軟體? lightdream1 . 0 。該軟體有效地實現了直升機實時飛行監控、機動飛行科目模擬和軌跡規劃及顯示等功能,滿足了無人直升機飛行控制系統的模擬需求。
  17. It has conducted an analysis of the virtual aircraft instrument system, finds out the characteristics of the system in flight simulator, and makes clear the data relationship between the virtual aircraft instrument system and other subsystems in flight simulator, including the function request as well as performance request for the system. with professional software vaps design the appearance of virtual aircraft instrument uses atn ( augment transition network model ) to develop the

    通過對整個虛擬航空儀表系統的需求分析,找到作為飛行模擬器虛擬航空儀表系統的自身特點,明確虛擬航空儀表系統和整個飛行模擬器及其它子系統之間的數據關系,結合航空儀表系統的實際應用確定虛擬航空儀表系統的功能要求和性能要求,確定虛擬航空儀表系統開發的整體方案和流程,最終開發整個飛行模擬器虛擬航空儀表系統。
  18. And then the stability and the stable error response of the dpll are analyzed. there is an obvious doppler shift frequency offset in the received signal with flight at a high speed, in the dissertation the uniform sampling second - order dpll is used to remove the frequency bias for its excellent high - pass characteristic of the error transfer function

    由於高速飛行的遙測目標在接收信號中會出現較大的多普勒頻率分量,而典型均勻采樣二階數字鎖相環dpll ( digitalphase - lockedloop )的誤差函數具有高通特性,所以本文提出一種利用其高通特性來去除多普勒頻率分量的新方法。
  19. With the develop of computer techniques, the digital autopilot system has replaced the analog system. the analog system has not been able to adapt the developmental desire of modem autopilot system function. the digital autopilot system, of which the computre is main part, has put up tremendous superiority in aspect of flight control system

    隨著計算機技術的發展,數字式飛行控制系統逐步代替了模擬式系統。模擬式系統已不能適應現代飛控系統功能發展的要求,而以計算機為主的數字式系統卻在飛行控制方面表現出其巨大的優越性。
  20. In the new guidance scheme, the flight trajectory restrained by a function of energy is tracked by commanding both the angle of attack and angle of bank

    控制攻角和傾斜角,用來跟蹤一由能量函數界定的飛行軌跡。該控制方案包括一個軌跡規劃器和一個控制律。
分享友人