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- Automatic Takeoff Thrust Control System 自動(dòng)起飛推力控制系統
- The parameters are optimized with respect to the tracking performances of missile control system and the criterions of side thruster control based on evolutionary strategies. 根據控制系統跟蹤性能要求和直接力控制原則，采用進(jìn)化策略對常規氣動(dòng)力控制器參數和模糊直接力控制規則進(jìn)行優(yōu)化設計。
- Electric control system of fiber drying section DK. 纖維干燥工段電控系統。
- Electric control system of sanding section DK. 砂光工段電控系統。
- The design of the flight control system with the vectored thrust is discussed. 對帶推力矢量飛機的飛控設計問(wèn)題進(jìn)行了研究。
- Electric control system of chips preparation and sifting secton DK. 木片制備及篩選工段電控系統。
- Study of source control system on golf electric vehicle. 高爾夫燃料電池電動(dòng)車(chē)電源控制系統研究。
- Results show that pintle could change the nozzle throat area and thus the motor pressure and thrust,which provided the capability for thrust control. 結果顯示喉栓能夠有效改變發(fā)動(dòng)機燃燒室壓力和推力,滿(mǎn)足發(fā)動(dòng)機推力控制要求。
- Disconnect the evaporation control system. 斷開(kāi)蒸發(fā)控制系統。
- Abstract: The design of the flight control system with the vectored thrust is discussed. 文摘:對帶推力矢量飛機的飛控設計問(wèn)題進(jìn)行了研究。
- Moreover,this paper also added two feedforward items into thrust control angles so as to eliminate the effect produced by the initial position and velocity errors. 同時(shí),在推力角中引入前饋?lái)?用于消除初始位置和速度偏差對軟著(zhù)陸的影響。
- This electric control system is used for harmonizing various units to work. 本機電氣控制部分用于實(shí)現各個(gè)裝置的協(xié)調工作。
- Experiment validated that this measure method can measure small thrust of electric thruster accurately. 實(shí)驗證明此測量方法可準確測得電推力器工作的小推力。
- Intelligent Monitor and Control System of Li-ion Battery for Electric Bicycle. 電動(dòng)助力車(chē)鋰離子電池組智能監控系統。
- Subsystems of flight control system II. 飛行控制系統的分系統2。
- To break factory's control system. 違反工廠(chǎng)各項管理制度;
- Delay tester for the remote control system. 遙爆延遲測試器。
- The permanent magnet linear synchronous motor (PMLSM) direct thrust control (DTC) system using space vector modulation (SVM) and sliding mode variable structure is analyzed in this paper. 對永磁直線(xiàn)同步電機(PMLSM)基于空間矢量調制和滑模變結構直接推力控制系統進(jìn)行仿真和實(shí)驗分析。
- The control system permits more flexibility. 控制系統允許有較大的變化。
- The results of the simulation indicate that the safety trajectory guidance strategy can achieve safety maneuver flying of the small satellite proximity operation when using thrust control method. 仿真計算結果表明，采用脈沖控制模式，本文提出的安全軌跡制導策略能夠實(shí)現小衛星臨近作業(yè)的安全機動(dòng)飛行。
