A new principle of dynamic flight simulation experiment for anti-aircraft weapon is presented for the simulation experiment of anti-aircraft weapon in laboratory. A mathematical model of obtaining the tagart truth values and a mathematical model of obtaining the truth values of pitch and roll positions of tracker are established. The dynamic flight simulation experiment principle and the mathematical models are verified through dynamic flight simulation experiment. The principle and the key technologies of simulating dynamic flight experiment are valuable for dynamic flight simulation experiment of anti-aircraft weapons, which will promote the research and development of new anti-aircraft weapons. The proposed method is used to establish the theoretical basis of the dynamic flying experimental system, which can be used for data processing and error analysis.
Key words
ordnance science and technology /
anti-aircraft weapon /
dynamic flight experiment /
truth value
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