Design of Sliding Mode Control System for a Feedback Linearisable Helicopter Nonlinear ModelDUAN Fu-hai, HE Chang-an1-4
Demands for Mixture Workability of Airport Pavement Rolling Compacted ConcreteHUANG Can-hua, LIU Xiao-jun5-8
Freqency Characteristic Analysis of an Aeroplane Hydraulic Source SystemXIAO Wen-jian, ZHU Qing-you, PAN Lu-yuan9-12
PC104 Bus Technology in the Aeronautic Testing InstrumentsYANG Jun-feng, ZHU Jia-hai, XIE Hong-xing13-16
The Analysis on Dispersion Characteristic of Aerial Defence Missile WarheadHE Guang-jun, WAN Shao-song, GAO Fu-li17-20
The Performance Evaluation of Synthetic Anti-jamming of Control and Guided Radar of Ground to Air Missile Weapon SystemCHEN Yong-ge, LIU Ming, GAN Min-zhu21-23
The Design and Application of Real Time Parallel Simulator for AeroenginesMA Cun-bao, PANG Zheng-she, SONG Dong, ZHANG Tian-wei28-30
The Relay Communication System of High Reliability Collected and Distributed ControlLI Jing-she, ZHANG Xiao-mu31-34
Methodology for Modeling and Simulation of Antiaircraft C3I SystemZHOU-Lin, LOU Shou-chun, ZHAO Jie, ZENG Jian-jun35-38