in-flight maneuver 中文意思是什麼
in-flight maneuver
解釋
機動飛行-
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。 -
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。 -
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。 -
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。 -
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。 -
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。
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