| ANALYTICAL MODEL OF HELICOPTER AIRCOMBAT AND MATHEMATICINVERSE SOLUTION |
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| 作者姓名： | Cao Yihua |
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| 作者单位： | Institute of Fluid Mechanics，Beijing University of Aeronauticsand Astronautics，Beijing，China，100083 |
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| 摘 要： | ＡＮＡＬＹＴＩＣＡＬＭＯＤＥＬＯＦＨＥＬＩＣＯＰＴＥＲＡＩＲＣＯＭＢＡＴＡＮＤＭＡＴＨＥＭＡＴＩＣＩＮＶＥＲＳＥＳＯＬＵＴＩＯＮＣａｏＹｉｈｕａ（ＩｎｓｔｉｔｕｔｅｏｆＦｌｕｉｄＭｅｃｈａｎｉｃｓ，ＢｅｉｊｉｎｇＵｎｉｖｅｒｓｉｔｙｏｆＡｅｒｏｎａｕ...
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ANALYTICAL MODEL OF HELICOPTER AIRCOMBAT AND MATHEMATICINVERSE SOLUTION |
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| Cao Yihua.ANALYTICAL MODEL OF HELICOPTER AIRCOMBAT AND MATHEMATICINVERSE SOLUTION[J].Chinese Journal of Aeronautics,1995(4). |
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| Authors: | Cao Yihua |
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| Abstract: | in helicopter air combat, the helicopter must have the maneuverability andagility to gain a firing position first and its weapon systems must be able to get firstround hits for successful air combat. In an attempt to address the questions, a generalanalytical model of helicopter / annament system combat is established. Taking the hel-icopter air combat at short range as an example, the kinematic law of a turreted gun iscalculated. The development and results here may provide a referable basis for maxinuz-ing the hit probability of the gun in air firing. |
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| Keywords: | helicopters maneuvers flight combat |
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