flight of idea 中文意思是什麼

flight of idea 解釋
思想奔逸
  • 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...
  • of : OF ＝Old French 古法語。
  • idea : n. 1. 主意；念頭；思想；計劃，打算；意見。2. 想像，模糊想法。3. 【哲學】理念，理性概念，觀念；【心理學】表像。4. 【音樂】主題，樂句，音型。
  1. Spinning flight of ballistic missile in boost phase is a new idea in order to penetrate laser ’ s interception. spinning missiles may be unstable due to dynamic and control interactions

    彈道導彈主動段自旋飛行是一種新的構想，旨在對抗激光武器攔截，實現主動段突防。
  2. Based on this main idea, first the thesis discusses the mathematics model of gyro and accelemeter, the initial alignment of north - pointed strapdown inertial navigation system, the method of calculation navigation, the method of generating flight orbit data, the method of ins / gps integrated navigation in detail. then the thesis develops the system generating flight orbit data and the system of real - time simulating strapdown inertial navigation with vc + + 6. 0

    論文以此為核心展開：首先詳細討論了陀螺和加速度計的數學模型、指北式捷聯慣性導航系統初始對準和導航解算的演算法、飛行軌跡數據生成演算法、 ins gps組合導航演算法；然後利用visualc + + 6 . 0開發出飛行軌跡數據生成系統、捷聯慣性導航實時模擬系統。
  3. The insurance time limit of boat idea a place difficult of access is from be stepped by insurance passenger carry on guarantee slip bright the port of airliner flight begins, to fly to till destination port walks out of port

    航意險的保險期限是從被保險乘客踏入保單上載明的航班班機的艙門開始，到飛抵目的港走出艙門為止。
  4. 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
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