maneuver thrust 中文意思是什麼

maneuver thrust 解釋
機動推力
  • maneuver : n. ,〈美國〉 =manoeuvre.
  • thrust : vt (thrust)1 猛推,沖;猛撳,沖入,插入,推入(出),突出,伸出,塞,刺,戳,戳穿。2 逼迫,把[...
  1. An on - line minimum - variance estimator was developed for thrust acceleration applied to orbit transfer using discrete - time radar measurements. the mass - flow - rate of propellant was selected as a state variant, which was estimated by employing an integral state model and ekf filter. the variation equations for measurement vector to mass - flow - rate have been established to linearize the discrete - time measurement equations. the algorithm has applied successfully to maneuver process in commanding satellite into geo - stationary orbit. the results show that the algorithm developed here can monitor and determine whether engine works well or failure precisely and quickly during orbit transfer process

    飛行器軌道機動過程中,為跟蹤、定位機動目標和干預機動控制過程,需要統計處理離散的雷達觀測量實時估計推進發動機的推力,進而確定飛行器的瞬時軌道參數.本文所述演算法是該工程問題的探討和解決方案.文章建立了軌道機動過程中連續變質量運動模型和離散雷達量測模型,推進發動機的質量秒耗量作為表徵推力加速度的一個近似常量,應用擴展卡爾曼濾波對離散的雷達測量數據進行順序統計處理給出秒耗量的最小方差估計;文章詳細地推導了線性化量測模型的變分方程和觀測矩陣;模擬結果表明該演算法能快速、準確地估計推進發動機的質量秒耗量和向機動目標施加的實際推力
  2. 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。
  3. 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。
  4. The results show that the fighter with thrust vector have smaller radius, shorter time and better maneuver performance

    結果表明,作戰飛機帶推力矢量后,完成半筋斗和加力盤旋機動動作的空間減小,時間縮短,機動性能得到了提高。
  5. The switch logic between high thrust and low thrust, switch rule between ppc methed and qsc methed, and the switch maneuver between pitching and attacking in af are given

    給出了高水平推力和低水平推力的切換邏輯,相平面控制與準滑模控制律的切換準則和角度反饋中俯仰角和攻角的切換策略。
分享友人