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- Here, we integrate both of them and propose reliable VSC control schemes to spacecraft attitude tracking problems. 另一方面，隨著(zhù)航空及工業(yè)界對可靠度的要求增加，有關(guān)可靠度控制的研究在這幾年也成為一個(gè)非常熱門(mén)的議題。
- 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。
- Topics extend to analysis of both aircraft flight dynamics and spacecraft attitude dynamics, based upon presented principles and equations of motion. 課題擴展分析了航天器飛行動(dòng)力學(xué)和太空船飛行姿態(tài)動(dòng)力學(xué)，這些建立在當前的運動(dòng)理論和方程式上。
- Reaction fly-wheel is the implementary element of the poser control system of the space vehicle.The control system of servo motor plays an important role in spacecraft attitude. 摘要反作用飛輪是航天空間飛行器姿態(tài)控制系統的執行機構，其驅動(dòng)電動(dòng)機伺服系統性能優(yōu)劣對飛行器的姿態(tài)有至關(guān)重要的作用。
- 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 steering laws of single gimbal control moment gyms (SGCMGs) are analyzed and compared for a spacecraft attitude control system based on the singular value decomposition (SVD) theory. 摘要基于奇異值分解理論，對航天器姿態(tài)控制系統中使用的單框架控制力矩陀螺(SGCMG)的操縱律進(jìn)行了分析和比較研究。
- ABSTRACT:Reaction fly-wheel is the implementary element of the poser control system of the space vehicle.The control system of servo motor plays an important role in spacecraft attitude. 摘要：反作用飛輪是航天空間飛行器姿態(tài)控制系統的執行機構，其驅動(dòng)電動(dòng)機伺服系統性能優(yōu)劣對飛行器的姿態(tài)有至關(guān)重要的作用。
- Abstract: In this paper,a sliding mode control(SMC) method is derived and applied to a spacecraft attitude tracking system in the presence of parameter variations and external disturbances. 文摘:對于參數不確定和外部擾動(dòng)的空間飛行器姿態(tài)跟蹤系統，本文提出了采用滑?？刂频姆椒?。
- spacecraft attitude stabilization 航天器姿態(tài)穩定
- Zero-disturbance spacecraft attitude 載體姿態(tài)無(wú)擾
- Cable control model for spacecraft attitude and vibrations 航天器姿態(tài)和振動(dòng)的拉索控制模型
- Spacecraft Attitude Determination by Using Infrared Horizon Sensors 基于紅外地平儀的航天器姿態(tài)確定技術(shù)
- The attitude of grownups has changed. 成年人的態(tài)度已有了轉變。
- The spacecraft is in orbit around the moon. 該航天器在繞月球軌道運行。
- The spacecraft was in its recovery mode. 這艘飛船處于返回狀態(tài)。
- He asked for help in a suppliant attitude. 他以懇求的態(tài)度要我幫忙。
- He has a mellow attitude to life. 他對生活有種成熟的看法。
- He undertook to defend this attitude. 他開(kāi)始為這一態(tài)度辯護。
- His attitude is antipathetic to me. 他的態(tài)度使我反感。
- QUASI-EULER-ANGLES FEEDBACK CONTROL OF SPACECRAFT ATTITUDE MANEUVER 航天器姿態(tài)機動(dòng)的擬歐拉角反饋控制
