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25 December 1985, Volume 6 Issue 6

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25 December 1985, Volume 6 Issue 6

APPLICATION OF ADAPTIVE CONTROL TO AIRCRAFT SYSTEMS
Abstract( 2227 )

Chen Zongji;Zhang Hongyue

1985, (6): 513-520.

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APPLICATION OF ROTOR INDUCED VELOCITY FIELD OF THE VORTEX THEORY TO THE STUDY OF STABILITY AND CONTROLLABILITY OF HELICOPTER WITH HINGELESS ROTOR
Abstract( 1452 )

Xin Zhiming;Wang Shicun

1985, (6): 521-529.

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ELASTOPLASTIC MATRIX IN NON-ORTHOGONAL CURVILINEAR COORDINATE SYSTEM
Abstract( 1309 )

Ren Xiaoan

1985, (6): 530-537.

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CALCULATION OF STRESS, STRAIN AND PLASTIC ZONE AHEAD OF CRACK TIP UNDER PEAK OVERLOAD WITH PULSATING LOADS BY ELASTOPLASTIC FEM
Abstract( 1028 )

Tang Xuanchun

1985, (6): 538-547.

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SOLUTION OF ELASTOPLASTIC CONTACT PROBLEM BY BOUNDARY ELEMENT METHOD AND MA- THEMATICAL PROGRAMMING TECHNIQUE
Abstract( 1251 )

Lu Shan

1985, (6): 548-555.

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IDENTIFICATION AND ESTIMATION OF THE RANDOM ERROR MODELS FOR INERTIAL ACCELEROMETER AND BARO-ALTIMETER
Abstract( 1668 )

Wang Renlin

1985, (6): 556-564.

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AN OPTIMAL PARAMETER ESTIMATION METHOD COMPATIBLE WITH STABSE PARAMETER PREDI CTIONN SN TIME DOMAIN
Abstract( 1132 )

Gan Hong;Wu Yaohua

1985, (6): 565-571.

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A GENERALIZED LEAST SQUARE METHOD WITH SPECIAL WHITENING FILTER
Abstract( 1693 )

Huang Junqin;Zhang Jizhi Miao Tong

1985, (6): 572-577.

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AN INERTIAL NAVIGATION SYSTEM WITH SINGLEE- AXILE-STABILIZATION
Abstract( 1328 )

Ren Sicong;Li Zongke

1985, (6): 578-584.

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A SECOND-ORDER THEORY FOR THREE-DIMENSIONAL UNSTEADY FLOWS AND ITS APPLICATION TO THIN WINGS WITH ANGLE OF ATTACK AT SUPERSONIC AND HYPE-RSONIC SPEEDS
Abstract( 1304 )

He Longde;Han Yanliang;Qian Fuxing

1985, (6): 585-589.

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FINITE ELEMENT ANALYSIS OF ELASTIC-PLASTIC MATERIALS BY “CONDENSED APPROACH”
Abstract( 1036 )

Ren Qiquan

1985, (6): 590-596.

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IMPROVEMENT OF SERVO SYSTEMS FOR FLIGHT SIMULATOR
Abstract( 1141 )

Sun Dezhi

1985, (6): 597-601.

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EFFECT OF SOME FACTORS ON THE FATIGUE THRESHOLD OF 30CrMnSiNi2A STEEL
Abstract( 1216 )

Zhao Wei;Ding Chuanfu;Gu Mingda;Yan Minggao

1985, (6): 602-609.

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