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- Automatic Takeoff Thrust Control System 自動起飛推力控制系統
- 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,採用進化策略對常規氣動力控制器參數和模糊直接力控制規則進行優化設計。
- Electric control system of fiber drying section DK. 纖維乾燥工段電控系統。
- 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題進行了研究。
- Electric control system of chips preparation and sifting secton DK. 木片製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車電源控制系統研究。
- 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動機燃燒室壓力和推力,滿足發動機推力控制要求。
- Disconnect the evaporation control system. 斷開蒸發控制系統。
- 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題進行了研究。
- 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,在推力角中引入前饋項,用於消除初始位置和速度偏差對軟著陸的影響。
- This electric control system is used for harmonizing various units to work. 本機電氣控制部分用於實現各個裝置的協調工作。
- Experiment validated that this measure method can measure small thrust of electric thruster accurately. 實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. 電動助力車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. 對永磁直線同步電機(PMLSM)基於空間矢量調製和滑模變結構直接推力控制系統進行模擬和實驗分析。
- 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. 模擬計算結果表明,採用脈衝控制模式,本文提出的安全軌跡制導策略能夠實現小衛星臨近作業的安全機動飛行。