Aerospace Control 1991 Issue S1 SEARCH FOR WAY OF GUIDANCE ACCURACY EVALUATION OF STRATEGIC MISSILE

SEARCH FOR WAY OF GUIDANCE ACCURACY EVALUATION OF STRATEGIC MISSILE
Xu yan wan Beijing Aerospoace Automatic Control Institute

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qian yan
dong ruo huan ;

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bian zhe de hua

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BALLISTIC MISSILE FLIGHT TEST AND ACCURACY EVALUATION
Zhao Shaokui

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

ANALYSIS ABOUT THE PROBLEM FOR GUIDANCE ACCURACY EVALUATION AND BALLISTIC IMPACT VERIFICATION OF INTERCONTINENTAL MISSILE
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
Wu Liren Beijing Aerospace Automatic Control Institute

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

SOME PROBLEMS OF APPLYING STATISTICAL TEST METHOD TO MISSILE ACCURACY EVALUATION
Wu Liren Beijing Aerospace Automatic Control Institute

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

APPLICATION OF THE IMPROVED LEAST SQUARE METHOD IN GUIDANCE ACCURACY ANALYSIS
Zhu Zhen-qian Beijing Aerospace Automatle Eontrol Institute

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

ADAPTIVE ESTIMATION OF THE INSTRUMENTAL ERROR TO THE GUIDANCE SYSTEM
Zhang Jin-Huai National University of Defense Technology

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

CONSISTENCE CHECK FOR GUIDANCE SYSTEM ERROR COEFFICIENTS BETWEEN FLIGHT TEST AND GROUND TEST
Liu lisheng

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

A NEW GUIDANCE ACCURACY CONVERSION METHOD USING LINEAR REGRESSION
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
Wu Ping Zhang Libin Luoyang Institute of Tracking and Telecommunications Technology

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

A CORRECTION METHOD FOR OPTIMAL LINEAR REGRESSION MODEL
Sha Yu Wang Zhengming Wu Yi National University of Defense Technology

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

STATISTICAL COVARIANCE METHOD AND COMPARISION WITH MONTE CARLO METHOD
Wang Yong Ping Beijing Aerospace Automatic Control lnsititute

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

SELECTION OF DATA REASONABLENESS CHECK AND ERROR SEPARATION METHODS
Cheng Guangxian Beijing Institute of Astronautical system Enginerring

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

A METHOD FOR JUDGING GROSS ERROR OF OBSERVATING DATA
Sha Yu Wang Zhengming National University of Defense Technology

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

SOME ANALYSES OF TIME ZERO POINT FOR TELEMETERING
Yang yanjun Wang qingmei Taiyuan Satellite Launching Complex

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

A METHOD TO OBTAIN HIGH ACCURACY TRAJECTORY POSITION PARAMETERS USING SELF-POSITION TECHNIQUE
Liu Lisheng Sun Lianqing Luoyang Institute of Tracking and Telecommunications Technology

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

MULTI-STATION TRACKING OPTIMAL ESTIMATES WITH SLIDING ARC
Xiao Jingyou

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

DEVELOPMENT AND IMPROVOMENT OF PRINCIPAL COMPONENTS ESTIMATION AND ITS APPLICATION IN THE SEPARATION OF GUIDANCE INSTRUMENTAL ERRORS
Sha Yu Wu Yi Wang Zheng Ming

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

ADAPTIVE SPLINE FILTERING METHOD FOR FIXING A VEHICLEORBIT
Tang Xue Mei National University of Defense Techonology

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

SEPARATING METHOD ON GUINDANCE ERROR COEFFICIENTS FROM EXTERIOR BALLISTIC MEASURING CHANNELS
Wu ping Zhang Libin Sun Liangqing Luoyang Institute of Tracking and Telecommunications Technology

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

REAL-TIME SELF-CALIBRATION OF INERTIAL PLATFORM
Yang Lixi Beijing Control Device Research Institute

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

ACCELEROMETER DYNAMIC MODEL IDENTIFICATION AND ERROR COMPENSATION
Xu Qiang Zheng Yuanxi Yuan Junan Beijing Control Devices Research Institute

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

AN APPLICATION OF AIRS TO ACCURACY EVALUATION OF MISSILES
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
Zhao Min Beijing Institute of Astronautical Systems Engineering

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