rapid maneuver 中文意思是什麼

rapid maneuver 解釋
快速機動
  • rapid : adj 1 快。2 敏捷的，麻俐的，快手快腳的（工人等）。3 峻險的（坡等）。4 【攝影】感光快的。n 〈常 pl...
  • maneuver : n. ,〈美國〉 ＝manoeuvre.
  1. Due to the size of the defect, a fragment of bone is introduced to support the mucosal graft. strength of the repair is verified by increasing intercranial pressure with the valsalva maneuver, and it is seen to be watertight. rapid - setting fibrin glue is applied, and a second layer of mucosa is applied over this

    由於瘺孔較大，置入一些骨的碎片以支持填塞物，通過valsalva法咽鼓管吹氣法增加顱內壓可以觀察修補的牢固性，可以看到沒有泄漏，利用可以快速固定的纖維蛋白膠進行固定，其上鋪上一層粘膜，然後再用膠水進行固定。
  2. The small astronomical satellite has demands on both pointing accuracy and attitude maneuverability, so this thesis modeled the attitude control subsystem based on reaction wheels. under the fine precision pointing mode, a pd control law and a variable structure ( vs ) control law were studied respectively, and the simulation validated that vs control is more effective under fine precision pointing mode. furthermore, the vs controller for rapid large - angle maneuver was also designed

    2 ） svom衛星同時對指向精度和姿態機動性有著很高的要求，因此本文建立了基於反作用飛輪的svom衛星姿態控制系統模型，在高精度慣性定向三軸穩定模式下分別設計了pd控制律和變結構控制律，通過模擬驗證了變結構控制對于svom衛星的有效性，並基於變結構控制研究了svom衛星快速大角度機動的方法。
  3. 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
分享友人
分享到 Line

分享到臉書