CONTROL THEORETIC APPROACH TO INERTIAL NAVIGATION SYSTEMS

被引:170
作者
BARITZHACK, IY
BERMAN, N
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D O I
10.2514/3.20299
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
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页码:237 / 245
页数:9
相关论文
共 14 条
[1]   IDENTITY BETWEEN INS POSITION AND VELOCITY ERROR MODELS [J].
BARITZHACK, IY .
JOURNAL OF GUIDANCE AND CONTROL, 1981, 4 (05) :568-570
[2]   COMPARISON OF 2 APPROACHES TO PURE-INERTIAL AND DOPPLER-INERTIAL ERROR ANALYSIS [J].
BENSON, DO .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1975, 11 (04) :447-455
[3]  
Britting K.R., 1971, INERTIAL NAVIGATION
[4]  
BROXMEYE C, 1964, INERTIAL NAVIGATION
[5]  
DAPPOLITO JA, 1971, AD881286
[6]  
GELB A, 1974, APPL OPTIMAL ESTIMAT, P79
[7]  
HELLER WG, 1975, TR3133 AN SCI CORP T
[8]  
HUTCHINSON CE, 1968, AD674526
[9]  
KWARKERNAAK H, 1972, LINEAR OPTIMAL CONTR, P65
[10]  
LEONDES CT, 1963, GUIDANCE CONTROL AER, pCH2