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- 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。
- 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。
- A novel method of fuzzy proportional-integral-differential (PID) control by GA is designed for the attitude control system of three-axis-stable mass moment missile in this paper. 摘要針對三軸穩定的質(zhì)量矩導彈姿態(tài)控制系統，提出了一種基于遺傳算法進(jìn)行參數尋優(yōu)的模糊PID控制方法。
- The spacecraft attitude control system is designed via a backstepping method,considering the attitude dynamic model on conditions that flywheels are adapted as actuatoss. 研究了航天器的姿態(tài)控制問(wèn)題?？紤]了飛輪作為執行機構的姿態(tài)動(dòng)力學(xué)模型,應用退步控制理論設計了姿態(tài)控制算法。
- The proper organic combination of the CMG control loop and DM control loop is the key of the overall forming of the BST gondola attitude control system. 這也使BST采用分級控制而獲得高分辨率太陽(yáng)圖像的科學(xué)觀(guān)測成為可能。
