1002-0853
2001 Issue 3
Application of Bayes theory in testing complicated hypothesis on modeling and simulation
zhao min rong ; liu xing tang ; wu xiao yan ; hui jian
zhao min rong ; liu xing tang ; wu xiao yan ; hui jian
..............page:84-86
LMI approach for determining the incremental-gain of saturated nonlinear system
zhao lu yang ; shi zhong ke ; li hua
zhao lu yang ; shi zhong ke ; li hua
..............page:80-83
Research on the equivalent compensation of IMU error before launching
xian yong ; qian pei xian
xian yong ; qian pei xian
..............page:77-79
Flight test of Z11 helicopter autorotation landing
niu yong hong ; yang bai xing
niu yong hong ; yang bai xing
..............page:74-76
Application of neural network dynamic inversion method in the flight control system design
li ai jun ; wang wei ; zhang wei guo ; shen yi
li ai jun ; wang wei ; zhang wei guo ; shen yi
..............page:70-73
..............page:66-69
Research on the warship-based helicopter's landing velocity on the surface of warship under regular surf
jia zhong hu ; gao yong ; guo wei gang
jia zhong hu ; gao yong ; guo wei gang
..............page:63-65
Application of adaptive fuzzy decoupled control for aircraft landing
wang ying jie ; shi zhong ke ; li hua
wang ying jie ; shi zhong ke ; li hua
..............page:60-62
Flight test research of aerodynamics pressure measurement technique for a delta-wing aircraft
chen zuo ; yu jun ya ; zhang de yuan ; meng jian wen ; huang wen jing
chen zuo ; yu jun ya ; zhang de yuan ; meng jian wen ; huang wen jing
..............page:56-59
Effectiveness analysis on cruise missile to anticraft missile
li qing zhen ; liu xin xue ; wang ming hai
li qing zhen ; liu xin xue ; wang ming hai
..............page:52-55
Research on TBM penetration ability in air-defense missile defense system
zhang yi ; he nian nian ; ma qing hua
zhang yi ; he nian nian ; ma qing hua
..............page:49-51
..............page:45-48
Optimal orbit maneuver of the space station adjoint satellite
luo jian jun ; li xin gang ; yuan jian ping
luo jian jun ; li xin gang ; yuan jian ping
..............page:41-44
An improved optimal guidance law and its simulation study
lian zuo hua ; cui ping yuan ; cui zuo tao
lian zuo hua ; cui ping yuan ; cui zuo tao
..............page:36-40
Helicopter inverse dynamic model based on neural network
huang wen ming ; xu jin fa ; gao zheng
huang wen ming ; xu jin fa ; gao zheng
..............page:33-35
Study on fault detection and aerodynamic model for control surface damage
zhang zuo zhe ; deng jian hua
zhang zuo zhe ; deng jian hua
..............page:28-32
Fuzzy adaptive post-stall flight control
hu meng quan ; wang jian pei
hu meng quan ; wang jian pei
..............page:24-27
Helicopter longitudinal dynamics modeling for highly-gain flight control system design
xu jun ; chen da rong ; wang jia dao ; chen zuo sheng
xu jun ; chen da rong ; wang jia dao ; chen zuo sheng
..............page:20-23
Study of combat agility management system
hu chao jiang ; zuo chong lou ; chen shi zuo
hu chao jiang ; zuo chong lou ; chen shi zuo
..............page:15-19
Comments on the new contents in performance provisions for certification of transport aircraft
huang wen jing ; wu mi cui ; wu ju ying
huang wen jing ; wu mi cui ; wu ju ying
..............page:12-14
Study of the present status and prospect of the guidance law
nie yong fang ; zhou qing ji ; zhang tao
nie yong fang ; zhou qing ji ; zhang tao
..............page:7-11
UCAV's development and key technologies
zuo xiang lin ; chen zuo
zuo xiang lin ; chen zuo
..............page:1-6