inertial guidance system 中文意思是什麼

inertial guidance system 解釋
慣性導航系統
  • inertial : adj. 【物理學】慣性的,慣量的。
  • guidance : n. 1. 向導,指引,指導。2. 導航;制導。3. 【機械工程】導槽,導板,導管。
  • system : n 1 體系,系統;分類法;組織;設備,裝置。2 方式;方法;作業方法。3 制度;主義。4 次序,規律。5 ...
  1. Aigs all inertial guidance system

    全慣性制導系統
  2. Taking intercontinental ballistic missiles as objects under research, and based on the analysis of the influence of accelerometer measurement error and gyroscope excursion error on the apparent acceleration, the error transfer model of the inertial system in a midcourse guidance segment for velocity and location is given, and the pure inertial navigation guidance error is computed with the given imu error coefficient deviations

    摘要針對洲際彈道導彈,在分析加速度計測量誤差和陀螺漂移誤差對導彈視加速度影響的基礎上,給出了中制導段慣性系統對速度和位置的誤差傳遞模型,對給定的慣組誤差系數偏差進行了純慣性導航制導誤差計算。
  3. Consequently, computational models of all subsystems are constructed, such as the strapdown inertial navigation system ( sins ), the control loop applied in self - control period, the guidance system by applying the technology of television ( tv ) guidance and the guidance law of proportion navigation, the autopilot by applying the technology of overload control in terminal control period, and so on

    建立導彈各個子系統的計算模型,主要有捷聯慣性導航系統、彈體、導彈自控段的控制穩定迴路、採用電視制導和比例導引制導律的導引系統,以及採用過載控制的自動駕駛儀,然後在此基礎上建立導彈各系統模擬模型。
  4. Inertial navigation and guidance are based on accelerometer sensitization and vehicle acceleration test, and the accelerometer precision influences the precision of navigation and guidance and operational performance of weapon system seriously

    慣性導航與制導以加速度計敏感、測量運載體加速度為基礎,加速度計的精度直接影響到導航與制導的精度和武器系統的作戰效能。
  5. Inertial gyros, which are universally applied to navigation system of various aircrafts, could reflect not only aerial attitude of aircrafts but also other important guidance information. as a result, it plays a key role in ensuring security and accuracy when controlling

    慣性陀螺儀普遍應用於各種飛行器的導航系統中,它反映了飛行器的飛行姿態以及其它重要導航信息,保證了對飛行器進行控制的安全性與準確性。
  6. All inertial guidance system

    全慣性制導系統
  7. Flight test analysis of an improved transfer alignment for missile strapdown inertial guidance system

    彈載捷聯慣性制導系統傳遞對準技術試飛驗證
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