Aerospace Control 1991 Vol. Issue S1

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航天控制
Aerospace Control

Year 1991

Issue S1

SEARCH FOR WAY OF GUIDANCE ACCURACY EVALUATION OF STRATEGIC MISSILE (战略导弹制导精度分析途径的探讨)

Xu yan wan Beijing Aerospoace Automatic Control Institute

.................. page:1-8

qian yan (前言)

DONG Ruohuan

.................. page:3

bian zhe de hua (编者的话)

.................. page:4

BALLISTIC MISSILE FLIGHT TEST AND ACCURACY EVALUATION (弹道导弹的飞行试验与精度鉴定)

Zhao Shaokui

.................. page:9-12

ANALYSIS ABOUT THE PROBLEM FOR GUIDANCE ACCURACY EVALUATION AND BALLISTIC IMPACT VERIFICATION OF INTERCONTINENTAL MISSILE (洲际弹道导弹制导精度鉴定和命中精度评定技术途径分析)

Zhu Zhenqian Beijing Aerospace Automatic control Institute

.................. page:13-21

STATE THE ROADS OF CHINA GUIDANCE ACCURACY EVALUATION FROM THE DEVELOPMENT PROCESS OF GUIDANCE ACCURACY EVALUATION OF U.S.A MINUTEMAN MISSILE (从美国民兵导弹制导精度鉴定的发展过程论我国制导精度鉴定的道路)

Wu Liren Beijing Aerospace Automatic Control Institute

.................. page:22-27

SOME PROBLEMS OF APPLYING STATISTICAL TEST METHOD TO MISSILE ACCURACY EVALUATION (导弹精度鉴定中应用统计试验法的几个问题)

Wu Liren Beijing Aerospace Automatic Control Institute

.................. page:28-33

APPLICATION OF THE IMPROVED LEAST SQUARE METHOD IN GUIDANCE ACCURACY ANALYSIS (改进最小二乘法在制导精度分析中的应用)

Zhu Zhen-qian Beijing Aerospace Automatle Eontrol Institute

.................. page:34-41

ADAPTIVE ESTIMATION OF THE INSTRUMENTAL ERROR TO THE GUIDANCE SYSTEM (制导系统工具误差的自适应估计)

Zhang Jin-Huai National University of Defense Technology

.................. page:42-54

CONSISTENCE CHECK FOR GUIDANCE SYSTEM ERROR COEFFICIENTS BETWEEN FLIGHT TEST AND GROUND TEST (制导系统误差系数天地因子的一致性检验)

Liu lisheng

.................. page:55-60

A NEW GUIDANCE ACCURACY CONVERSION METHOD USING LINEAR REGRESSION (运用线性回归进行制导精度折合)

Jia peiran Wang mingxin Zhao zhijian National University of Defense Technology

.................. page:61-73

COMPACT LEAST SQUARE ESTIMATION AND PARAMETER SEPARATION OF LINEAR REGRESSION MODELS (线性回归模型的紧致最小二乘估计及参数分离)

Wu Ping Zhang Libin Luoyang Institute of Tracking and Telecommunications Technology

.................. page:74-84

A CORRECTION METHOD FOR OPTIMAL LINEAR REGRESSION MODEL (最优线性回归模型的校正)

Sha Yu Wang Zhengming Wu Yi National University of Defense Technology

.................. page:85-92

STATISTICAL COVARIANCE METHOD AND COMPARISION WITH MONTE CARLO METHOD (统计协方差方法及其与蒙特卡洛法的比较)

Wang Yong Ping Beijing Aerospace Automatic Control lnsititute

.................. page:93-103

SELECTION OF DATA REASONABLENESS CHECK AND ERROR SEPARATION METHODS (数据的合理性检验与误差分离方法的选择)

Cheng Guangxian Beijing Institute of Astronautical system Enginerring

.................. page:104-111

A METHOD FOR JUDGING GROSS ERROR OF OBSERVATING DATA (判断观测数据过失误差的方法)

Sha Yu Wang Zhengming National University of Defense Technology

.................. page:112-120

SOME ANALYSES OF TIME ZERO POINT FOR TELEMETERING (遥测时间零点的分析)

Yang yanjun Wang qingmei Taiyuan Satellite Launching Complex

.................. page:121-124

A METHOD TO OBTAIN HIGH ACCURACY TRAJECTORY POSITION PARAMETERS USING SELF-POSITION TECHNIQUE (应用自定位技术提供高精度的弹道位置参数)

Liu Lisheng Sun Lianqing Luoyang Institute of Tracking and Telecommunications Technology

.................. page:125-131

MULTI-STATION TRACKING OPTIMAL ESTIMATES WITH SLIDING ARC (多站可变弧段直接最佳弹道估计)

Xiao Jingyou

.................. page:132-135

DEVELOPMENT AND IMPROVOMENT OF PRINCIPAL COMPONENTS ESTIMATION AND ITS APPLICATION IN THE SEPARATION OF GUIDANCE INSTRUMENTAL ERRORS (主成分估计的发展和完善及其在制导工具误差分离中的应用)

Sha Yu Wu Yi Wang Zheng Ming

.................. page:136-146

ADAPTIVE SPLINE FILTERING METHOD FOR FIXING A VEHICLEORBIT (飞行器定轨中的自适应样条滤波方法)

Tang Xue Mei National University of Defense Techonology

.................. page:147-154

SEPARATING METHOD ON GUINDANCE ERROR COEFFICIENTS FROM EXTERIOR BALLISTIC MEASURING CHANNELS (外测通道域的制导误差分离法)

Wu ping Zhang Libin Sun Liangqing Luoyang Institute of Tracking and Telecommunications Technology

.................. page:155-160

REAL-TIME SELF-CALIBRATION OF INERTIAL PLATFORM (惯性平台的实时自校准)

Yang Lixi Beijing Control Device Research Institute

.................. page:161-176

ACCELEROMETER DYNAMIC MODEL IDENTIFICATION AND ERROR COMPENSATION (加速度表动态模型辨识和误差补偿)

Xu Qiang Zheng Yuanxi Yuan Junan Beijing Control Devices Research Institute

.................. page:177-184

AN APPLICATION OF AIRS TO ACCURACY EVALUATION OF MISSILES (高级惯性参考球在导弹精度鉴定中的作用)

Song Xubing Xie Yighe Beijing Control Device Research Institute

.................. page:185-189

PROCESS OF TRANSLATED GPS TRACKING MEASURING DATA AND ANALYSIS OF STATE EVALUATION METHODS (转发GPS外测数据处理及状态估计方法分析)

Zhao Min Beijing Institute of Astronautical Systems Engineering

.................. page:190-202

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