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- AACS Active Attitude Control System 主動(dòng)姿態(tài)控制系統
- The attitude control system of maneuver missile head is designed by applyi ng nonlinear decoupling control law. 然后采用非線(xiàn)性解耦控制理論設計了機動(dòng)彈頭的姿態(tài)控制系統。
- To enhance the robustness of interceptor attitude control system, a switch control method is presented to control the attitude of interceptor. 摘要為增強攔截器姿態(tài)控制系統的魯棒性,提出了一種切換控制方法來(lái)控制攔截器的姿態(tài)。
- The Attitude Control System( ACS) software is responsible for maintaining the attitude of the spacecraft. 姿態(tài)控制系統(CS)件負責維護航空器的姿態(tài)。
- The attitude control system (ACS) ensures the satellite to keep running normally. 摘要姿態(tài)控制系統是衛星得以持續正常工作的保證。
- The integrated power and attitude control for a bias momentum attitude control system is investigated. 研究偏置動(dòng)量姿態(tài)控制系統中的集成能量與姿態(tài)控制問(wèn)題。
- Flywheel is an important executive component of satellite attitude control system. 飛輪是衛星姿態(tài)控制系統的關(guān)鍵執行元件。
- The suspension damping control strategy for vehicle attitude control system is presented. 提出了車(chē)輛姿態(tài)控制系統的懸架阻尼控制策略。
- The improvement of flywheel control system is spurred by high performance satellite attitude control system. 提高飛輪控制系統的性能對衛星姿態(tài)控制系統具有重要意義。
- This dissertation studies the applications of backstepping control design method on spacecraft attitude control system. 本論文研究退步控制設計方法在航天器姿態(tài)控制系統中的應用問(wèn)題。
- A.Kawaji, F.Arai, and T.Fukuda, “3D attitude control system for bio-micromanipulation,” IEEE, pp. 197-202, 2001. 陳泰成,“微組裝系統影像伺服建模與測試”,國立成功大學(xué)機械工程學(xué)系論文,中華民國九十一年。
- The attitude control system(ACS) ensures the satellite to keep running normally. 姿態(tài)控制系統是衛星得以持續正常工作的保證。
- Abstract :The problems concerning an aerospace vehicle’s (ASV) atmospheric reentry flight attitude control system were researched. 摘要 :研究了空天飛行器(ASV)再入跨大氣層飛行時(shí)的姿態(tài)控制問(wèn)題。
- Active Attitude Control for a Spin Stablized Spacecraft while Flying Freely 自由飛行態(tài)主動(dòng)式自旋穩定姿態(tài)控制
- The stratospheric nacelle attitude control system is the key technology in keeping position stabilization and posture adjustment. 摘要氣球吊籃姿態(tài)控制系統是吊籃在空中保持姿態(tài)穩定、進(jìn)行姿態(tài)調整的關(guān)鍵部件。
- Then,the interceptor has to maneuver with large angles and in this time the attitude control system is a nonlinear,MIMO,coupled system. 在這種情況下,攔截器必須進(jìn)行大角度姿態(tài)機動(dòng)。這時(shí)的姿態(tài)控制系統是一個(gè)非線(xiàn)性、多輸入多輸出耦合控制系統。
- A large flexible vehicle with tank using reaction jet attitude control system(ACS) design is a very complex and important problem. 通過(guò)數學(xué)仿真表明,形狀輸入法和合理的脈沖調寬邏輯可以有效抑制大撓性飛行器姿態(tài)機動(dòng)控制過(guò)程中的撓性振動(dòng)。
- During the early stage of reusable launch vehicle(RLV) re-entry flight,reaction control system(RCS) is a major attitude control device. 可重復使用航天器再入過(guò)程初期,反作用力控制系統是其姿態(tài)控制的主要手段,結合氣動(dòng)舵面可以減小飛行器對該系統的總沖需求,提高飛行器動(dòng)態(tài)響應特性。
- The problems concerning an aerospace vehicle's (ASV) atmospheric reentry flight attitude control system were researched. 摘要研究了空天飛行器(ASV)再入跨大氣層飛行時(shí)的姿態(tài)控制問(wèn)題。
- It's an active attitude, which usually brings good results. 這是一種積極的態(tài)度,這種態(tài)度往往會(huì )帶來(lái)好的結果。