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25 November 1993, Volume 14 Issue 11

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25 November 1993, Volume 14 Issue 11

论文

A STUDY OF THE AIRPLANE PRECISION LANDING APPROACH UNDER GUIDANCE OF GPS/INS
Abstract( 1349 )

Gu Lei;Xiao Ye-lun

1993, (11): 561-568.

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INTERVAL ESTIMATION AND HYPOTHESIS TEST FOR PERCEN-TILES AND PERCENTAGES OF CONTINUOUS DISTRIBUTIONS
Abstract( 1413 )

Fu Hui-min

1993, (11): 569-577.

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THEORY OF INCOMPLETE DATA RANK DISTRIBUTIONS
Abstract( 1174 )

Fu Hui-min

1993, (11): 578-584.

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A TIME DOMAIN METHOD FOR PROPELLER NOISE PREDICTION INCLUDING AIRCRAFT FUSELAGE EFFECT
Abstract( 1671 )

Li Xiao-dong;Sun Xiao-feng;Hu Zong-an;Zhou Sheng

1993, (11): 585-591.

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STUDY ON DYNAMIC PROPERTIES OF A ROTOR-GEAR INTERACTIVE SYSTEM
Abstract( 1210 )

Li Yan;Kuang Wei

1993, (11): 592-595.

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ERROR-CORRECTING CODES AND NEURAL NETWORKS
Abstract( 1469 )

Xiu da-zhuan;Wang Yong-chen

1993, (11): 596-600.

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A NEW APPROACH TO STABILIZATION OF TETHERED SATELLITES DURING STATION KEEPING
Abstract( 1206 )

Ji Ying-cun;Gao Wei-bing

1993, (11): 601-611.

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STUDY ON THERMAL EXPANSION COEFFICIENT AND DESIGN FOR ZERO-EXPANSION OF SINGLE ANDHYBRID MULTI-DIRECTIONAL COMPOSITE
Abstract( 1441 )

Zhong Wei-hong;Zhang Zuo-guang;Song Huan-cheng

1993, (11): 612-617.

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A METHODOLOGY FOR THE COMPREHENSIVE EVALUATION AND SELECTION OF AIRCRAFT AND ITS SENSITIVITY ANALYSIS OF PRIORITY
Abstract( 1571 )

Guan Jian-cheng Xia Yun-lu

1993, (11): 618-624.

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AERODYNAMIC INVESTIGATION ON INTERACTION OF VORTEX WITH STATIONARY AIRFOIL
Abstract( 1334 )

Li Feng;Wang Yi-yun;Cui Er-jie

1993, (11): 625-628.

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AN APPLICATION OF LINEAR GMRES ALGORITHM FOR SOLVING FULL POTENTIAL EQUATION
Abstract( 2130 )

Wu Yi-zhao

1993, (11): 629-631.

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NUMERICAL SIMULATION OF FLOWS PAST A LONGITUDINALLY OSCILLATING AIRFOIL AT HIGH INCIDENCES
Abstract( 1863 )

Lu Xi-yun;Zhuang Li-xian;Yin Xie-yuan;Tong Bing-gang

1993, (11): 632-635.

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THE CLOSED-FORM SOLUTION TO GUIDANCE PROBLEM
Abstract( 2484 )

Jiang Yu-xian

1993, (11): 636-639.

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THEORETICAL AND EXPERIMENTAL INVESTIGATION OF SEMI-ACTIVE CONTROL OF STRUCTURAL NONLINEAR FLUTTER
Abstract( 2061 )

Yang Zhi-chun;Zhao Ling-cheng;Jiang Jie-sheng

1993, (11): 640-643.

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APPLICATION OF EBE STRATEGY IN STRUCTURAL ANALYSIS -EBE-CG METHOD AND ITS PARALLEL IMPLEMENTATION
Abstract( 2277 )

Zhou Shu-quan;Deng Shao-zhong

1993, (11): 644-648.

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A POLARIZATION-SELECTIVE REFLECTOR ANTENNA WITH SMALL RCS
Abstract( 2115 )

Feng Lin;Lei Ping;Ruan Ying-zheng

1993, (11): 649-652.

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A FUZZY MODEL FOR SOFTWARE RELIABILITY VALIDATION
Abstract( 1752 )

Cai Kai-yuan

1993, (11): 653-656.

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TRANSFER ALIGNMENT OF INERTIAL UNITS ON ELASTIC BODY
Abstract( 2167 )

Zhang Hong-yue;Zhang Hong-hua

1993, (11): 657-661.

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A STUDY OF THE FAULT-TOLERANT CONTROL FOR PLANT IN OPERATIONAL PROCESSES
Abstract( 1936 )

Wang Zhong-sheng

1993, (11): 662-665.

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COMPUTATION OF THE WEIGHTS IN THE RATIONAL BEZIER CURVES
Abstract( 1146 )

Jiang Da-wei;Gou Qing-dong

1993, (11): 666-669.

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PARTICLE IMAGE CINEMATOGRAPH VELOCIMETRY
Abstract( 1146 )

Shen Gong-xin;Ma Guang-yun

1993, (11): 669-670.

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SEM IN SITU OBSERVATION OF THE TENSILE FRACTURE BEHAVIOR INAN Al-Li-Cu-Mg-Zr ALLOY
Abstract( 1128 )

Zhen Liang;Mao Jian-fu;Sun Dong-li;Yang De-zhuang

1993, (11): 670-672.

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