flight control law 中文意思是什麼
flight control law
解釋
飛行控制規律-
The guidance scheme includes a trajectory planner that generates a feasible flight trajectory and a control law that achieves bounded tracking of the downrange and crossrange distances as functions of energy
其中，軌跡規劃器可產生一個可行的飛行軌跡。控制律作為能量的函數可實現再入段對縱向和橫向航程的有界跟蹤。 -
Lqr lqt in design of flight control law
輸出反饋在飛行控制律設計中的應用研究 -
Aircraft flight dynamic and envelope protection control law in smart icing system are researched in this thesis
本文對結冰飛行動力學特性及智能防冰系統中的包線保護控制律設計問題進行了研究。 -
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。 -
On the basis of these, a simplified iced aerodynamics model is established, describes the effects of aircraft icing on aerodynamic parameters. main principle and implement method of iced aircraft envelope protection system are proposed. after ascertain iced aircraft envelope, for pilot and autopilot, open - loop and close - loop aircraft envelope protection control law respective designed, ensure the aircraft will efficiently follow the flight path specified by the pilot in the safe - flight envelope
在此基礎上，建立了簡化的飛機結冰氣動模型，以描述結冰對氣動參數的影響;給出了結冰飛行包線保護系統的基本原理及實現方法，在計算確定結冰飛行包線后，對於人工駕駛、自動駕駛飛行兩種情況，分別設計了開環、閉環飛行包線保護控制律，保證飛機在安全飛行包線內沿著預定的航線飛行。 -
Study on the advanced approaches for clearance of modern flight control law
現代飛行控制律評估與確認先進方法研究 -
The objective of this thesis is to design an artificial neural network adaptive reconfigurable flight control law basing on the view of engineering and to establish a flight simulation system with normal aircraft, fault aircraft, normal flight control law, reconfigurable flight control law and fault verification by c + + program
本文目的是從工程角度考慮，重點開發神經網路自適應的自修復重構飛行控制律。並在c + +環境下建立具有正常與故障飛機、正常與自修復重構飛行控制律和故障認定等模塊的飛行綜合模擬系統。 -
Using this method, the flight control law which suits to the vectored aircraft flight in post - stall domain is designed in this paper
運用這種方法對推力矢量飛機進行了適用於過失速機動的非線性飛行控制系統設計。 -
First, to research the reconfigurable flight control system, a flight simulation system of normal aircraft with normal flight control law is established
首先，為了自修復飛行控制系統研究，建立了具有正常飛行控制律的正常飛機飛行模擬系統。 -
The uav can fly along the scheduled fight path with correct attitude by the research of the control law of portrait flight track and transverse coordinated turn
文中通過研究無人機縱向航跡跟蹤和橫側向協調轉彎的控制律使得無人機可以以下確的姿態沿預定的航跡飛行。 -
Failure detection and isolation ( fdi ) is the key technique of srfcs, which can forecast the occurrence of potential failure, tell why and where it occurs, and then provide relevant information for trigger test, control law reconfiguration and automated maintenance diagnostic. flight control law reconstruction is the another core
故障檢測與隔離是自修復飛控系統的核心技術之一，它能及時判斷故障發生的原因和部位，預測潛在故障的發生，進而為及時預警以及進行飛行控制律重構和自主維護診斷提供相關信息和依據。 -
It was analyzed about the problems of space vehicle flight control, the development of space vehicles, the design aim and main characteristic of flight control systems of varied space vehicles, the main design requirement of flight control system of reusable space vehicles, the key technology which have to be resolved in flying control law design and flight control system design
摘要分析了空間飛行器飛行控制系統要解決的問題，空間飛行器的發展過程，各類空間飛行器飛行控制系統設計目的和主要特點，可重復使用的發射飛行器飛控系統的主要設計要求，在設計要求的確定，飛行控制律設計和飛行控制系統設計中要解決的關鍵技術。 -
The application of control law developed above to the problem of reconflgurable flight control is described. based on the simulation results, the effects of learning rate ( or adaptation gain ) and slide model terms on the control system are discussed. comparing with adaptive control, the control law is helpful to improve system ' s transition response and reduce undesirable oscillations, provides nearly perfect tracking in the case of undetected failure
4 、探討了所設計的控制律在重構飛行控制中的應用，討論了自適應調整率對自適應控制性能的影響、滑模魯棒控制補償項對控制性能的影響；對幾種舵面損傷的模擬結果表明，本文的控制律較自適應控制具有響應改善速度快、響應振蕩小的優點，具有較好的重構功能。 -
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。 -
Based on the flight datum of a300, the mathematical models and the normal control law of uav are built. separating the traditional flight control surfaces into several independent portions, we can reduce the influence of the control surface each and add redundance to the systems at the meanwhile
採用將傳統操縱面分離成為各自獨立的操縱面的方法，提高了操縱面的綜合作用效果，因而使無人機具有了傳統飛機所沒有的操縱面控制冗餘。 -
In follow, nonlinear six - degrees - freedom uav dynamic model is built, that is base of flight simulation. arithmetic in matlab simulation is analyzed. uav flight control law and navigation mode are given
其次，建立了無人機從發射到傘降回收的十二階s - function非線性飛行動力學模型，並對其模擬演算法進行了分析。 -
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。 -
With the increasing demand of unmanned aerial vehicle ( uav ) in military application, it is more and more important to develop flight control system techniques of uav. simulations are widely applied on present researches of flight control systems. uav flight control law and digital simulation research for flight envelope with matlab tools is the center of this thesis
飛行控制技術研究的主要手段是模擬和試驗，本文配合某型低速無人機飛行控制系統的研製工作，以matlab為工具，對無人機飛行控制律和全過程飛行模擬技術進行了研究。 -
It includes esm and t - esm and some flying quality evaluating laws such as the bandwidth law ( bwl ), the neal - smith law ( nsl ), the chalk law ( cl ) and the c * law. this software is useful for the design of flight control systems
該軟體包可以用頻域等效系統方法、時域等效系統方法、帶寬準則、閉環準則、俯仰角速率準則、 c準則等進行飛行品質的計算及評估，對飛控系統設計有實用價值。 -
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。
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