1673-1220
2002 Issue 3
zhi sheng ji zai xi bu da kai fa zhong de qiang xian jiu sheng he yi liao jiu hu
zou yuan zhen ; xiao jing
zou yuan zhen ; xiao jing
..............page:47-51
ADAPTIVE NONLINEAR CONTROL OF AN UNMANNED HELICOPTER
ge tie ; hu tao
ge tie ; hu tao
..............page:33-36
..............page:25-28
zhi sheng ji fa dong ji shu zi kong zhi xi tong jian shu
li jia yun ; chen hua
li jia yun ; chen hua
..............page:43-46
..............page:52-54
MILITARY HELICOPTER BATTLED DAMAGE ASSESSMENT AND REPAIR
chen sheng bin ; xu you cheng
chen sheng bin ; xu you cheng
..............page:37-42
THE DESIGN OF MESUREMENT AND CONTROL SYSTEM OF SOME TYPE HELICOPTER\'S INTEGRATED TEST BENCH
liu fu hua ; chen de jun
liu fu hua ; chen de jun
..............page:16-19
THE RESEARCH OF THE POSITIVE OR NEGATIVE PRESSURE IS USED TO SIMULATE THE FUEL OVERLOADING IN THE GROUND SIMULATED TEST OF HELICOPTER FUEL PUMP SELF-SUCKING
yang xiao long ; xiong zhang lin ; li jia yun
yang xiao long ; xiong zhang lin ; li jia yun
..............page:20-24
THE CHARACTER OF KA-28 HELICOPTER AND ITS COAXIAL TWIN ROTOR SYSTEM
fu bai xian ; zhao wei yi ; liu hang ; bi yu quan
fu bai xian ; zhao wei yi ; liu hang ; bi yu quan
..............page:12-15
..............page:6-11
RESEARCH OF KEY TECHNICAL PROBLEMS ABOUT ATTACK HELICOPTER AIR-COMBAT
zeng guo gui ; jiang chang sheng
zeng guo gui ; jiang chang sheng
..............page:29-32
RESEARCH ON TAIL ROTOR SPOT TURN LOAD CALCULATING OF HELICOPTER
cai hui lian ; zuo feng
cai hui lian ; zuo feng
..............page:1-5