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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1998, Vol. 19 ›› Issue (3): 361-364.
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Wang Yunchang
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Abstract:
This paper presents a mathematical model of a fire control system. With the information provided by plane canned radar and the sensors, the target velocity V t and the input aspect angle Q are determined. A method based on the linear extrapolation and analytic revision is used to calculate the maximum and minimum allowable launching range.Finally the result of simulation is given. This model has been used in a modified radar fire control system of an active high altitude,high speed fighter.
Key words: fire- control syst ems, missile launching r ange, computers
CLC Number:
TJ765.2
V249
Wang Yunchang. AIR TO AIR MISSILE FIRE CONTROL MATHEMATICAL MODEL APPLIED TO MODERN AIRPLANE FIRE CONTROL SYSTEMS[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1998, 19(3): 361-364.
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