flight maneuver 中文意思是什麼
flight maneuver
解釋
特技飛行-
The helicopter is allowed to fall the same distance that it climbed at the beginning of the maneuver before pulling the helicopter back to straight and level flight
待直升機垂直俯沖的距離與垂直爬升的距離相同時，拉起機頭恢復成水平直線飛行。 -
Finally, the thesis developed 3d animation flight simulation platform for helicopter using opengl in visual c + +. and the 3d terrain and helicopter model are constructed. the simulation of two typical maneuver ( s maneuver flight and bopup - bopdown ) and terrain following shows that the fight control system of attack helicopter is improved by the realistic optical impact
本文最後在vc環境下用opengl開發了直升機三維動畫模擬平臺，構造了三維地形和直升機模型，模擬了直升機做蛇形機動、急躍升急躍降、地形跟隨等機動飛行，通過逼真的視覺效果驗證了飛控系統的正確性。 -
In addition, a series of reasonable time histories of helicopter velocity, angular velocity and flight attitude were shown during the given dolphin maneuver flight
最後以黑鷹直升機為例計算了魚躍越障機動飛行時駕駛員操縱輸入及直升機速度、角速度和飛行姿態的變化規律。 -
The caution message cut the flight short, but we still managed to perform some of the planned maneuver blocks, which included throttle transients and one - half stick and pedal inputs
這個警告信息使得飛行時間被縮短了，但我們仍然安排完成了一些計劃中的飛行動作，其中包括節流閥瞬變、半桿操作和方向舵操作。 -
Due to mission profile, launched conditions and trajectory, maneuver chains for stand off missile are designed. instruction control model and maneuver model is setup for ucav flight simulation
結合作戰任務剖面、導彈發射條件和彈道，設計出無人機防區外攻擊導彈發射前、后的機動動作鏈。 -
Nowadays, squeeze film dampers ( sfd ) are used to reduce the vibration in many aero - engines, and then their performance in maneuver flight will affect the whole engine
現今，有不少航空發動機都採用了擠壓油膜阻尼器來減小發動機的振動，而擠壓油膜阻尼器在機動過載的作用下的運動特性將對發動機轉子產生重要影響。 -
For researching the flight test techniques of thrust vector controlled aircraft, dynamic models of thrust vector controlled aircraft were established, four post stall maneuver control laws were designed with the dynamic inverse method, tested and investigated according to a standard evaluation maneuver set ( stems )
摘要為研究推力矢量飛機的試飛技術，建立了推力矢量飛機的動力學模型，用動態逆方法設計了4種過失速機動控制律，並在地面飛行模擬器上參考標準評估機動動作集（ stems ）進行了飛行模擬試驗研究。 -
Thrust vectoring is the key technique for the modem fighter with agility and post - stall maneuver ability and good flight quality. and now it is the necessary technique for the fourth generation fighter and hot technique for the performance improvement for the third generation fighter
推力矢量技術是現代戰機具有敏捷性、過失速機動能力、良好的飛行品質的關鍵技術，其已成為第四代戰斗機的必備技術和第三代戰斗機改型的熱門技術，得到了越來越多的重視。 -
In this paper involved several aspects about the inner and outer loops design for helicopter flight control system, maneuver flight simulation for helicopter, terrain following simulation and 3d animation flight simulation system designed with opengl
主要的內容包括直升機飛行控制系統內外迴路設計、直升機機動飛行的模擬、地形跟隨的模擬以及opengl三維動畫模擬等方面的內容。 -
Abstract : this paper presents an inverse simulation algorithm of determining the pilot control law as well as the time histories of helicopter velocity, angular velocity and flight altitudes to follow a given helicopter maneuver flight path
文摘:本文給出了一種直升機機動飛行的逆模擬方法以計算跟隨預定飛行軌跡的駕駛員操縱。 -
According to the study above, we bring forward combined rbf - rbf neural network to target assignment and attack sequence decision, which is proved to be feasible by matlab simulation. thirdly, we build mathematics model of super - maneuver fighter and part the aircraft states to two loops based on principle of time delay. then nonlinear dynamic inverse theory is applied to design the flight control law
接下來本文建立了超機動飛機的數學模型，並根據時標分離的原則，將飛機狀態劃分為快迴路和慢迴路，然後應用非線性動態逆理論分別構造兩個迴路的控制律，同時利用設計的飛控系統對赫布斯特機動進行了模擬。 -
Under the requirement of multi - maneuver flight mission, spacecraft sometimes has to perform autonomous navigation by using on - board sensors in a short time
未來多任務航天器往往要執行多次機動飛行，由於地面導航的局限性，需要在較短的時間內對航天器進行自主導航。 -
First of all, it is devoted to discuss the open - loop characteristics and the nonlinear bifurcation analysis and the maneuver ability for the super - maneuverable flight nonlinear model of the new generation fighter. then a flight control system is designed in analytical dynamical inversion method based on the time - scale separation principle
首先，對新一代殲擊機超機動飛行的非線性模型的開環特性、分叉特性及機動能力進行分析，並以此模型為基礎，採用基於時標分離原則的動態逆控制方法設計了新一代殲擊機的飛行控制系統。 -
Abstract : two computational techniques for inverse fight dynamics, namely derivation - iteration and integration - iteration techniques, are investigated. the application of inverse dynamics to determine control power requirements for post - stall maneuvering is researched, and a maneuvering flight trajectory based algorithm is provided, which lays a numerical foundation for simplifying design criteria for post - stall aircraft. with the model of inverse dynamics employed, a flight control mode for the outermost loop of the control system, named maneuver generator, is designed to follow desired complicated maneuvering flight trajectories. an example of rapid heading - reversal maneuver and other numerical simulations show the feasibility of the algorithm and the design idea
文摘:考察了求解輸入類飛行逆動力學問題的微分-迭代與積分-迭代演算法;探討了利用逆動力學確定過失速機動操縱效能要求問題，這構成了進一步提出過失速機動飛機設計簡化判據的數值基礎;利用逆動力學設計機動發生模塊進行飛控系統的最外環控制，以便跟蹤期望的復雜機動軌跡.飛機最速反向示例及其它數值模擬結果表明設計思想與演算法是可行的 -
The design of wavelet neural - networks flight control system for helicopter is studied in this dissertation, which involving several aspects about building flight dynamics nonlinear model for helicopter, inverse dynamic design for helicopter flight control system, compensating inverse error by wavelet neural - networks and maneuver flight simulation for helicopter
本文就小波神經網路控制在直升機飛行控制系統中的應用進行了深入的研究和探索，主要的內容包括直升機飛行動力學非線性數學模型的建立、飛行控制系統的動態逆設計、小波神經網路對動態逆誤差的補償及直升機機動飛行模擬等方面的內容。 -
Nonlinear dynamic inversion control law can better solved the control problem of super - maneuver flight. consider the engineering implement and the idiographic request of air force equipment department, this thesis used c + + programming language to describe dynamic inversion control law and model of the fourth generation fighter. for the convenience of user interface and maintenance, we encapsulated the software as a dll
考慮到工程實現和空軍裝備部的具體要求，本文採用c + +語言來對動態逆控制律以及第四代殲擊機模型進行描述，為了用戶介面和維護的方便，在此基礎上使用dll動態鏈接庫的形式對軟體進行了封裝。 -
Design method of fuzzy system to control large maneuver flight of aircraft
飛機大機動飛行的一種模糊控制系統設計方法 -
Simulation that is the developing of the flight dynamics of helicopter is the best way to study maneuver flight of helicopter
計算機模擬是研究直升機機動飛行最有力的手段，直升機模擬技術也是直升機飛行動力學發展的方向之一。 -
In order to ensure the stable work of fighter planes while increasing their maneuverability, it is necessary to investigate the vibration performance of aero - engine in maneuver flight
為了確保飛機在提高其機動性能的同時還能穩定工作，不發生故障，有必要對機動飛行條件下的發動機轉子系統的振動特性進行研究。
分享友人