摘要
Aim To study the effect of aerodynamically stabilized seeker dynamics on guided bomb system analysis. Methods A thorough analysis of aerodynamically stabilized seeker dynamics was made to show that because of the much smaller time constant, its dynamic model can be greatly simplified. Results and Conclusion In guided bomb guidance/control digital simulation, with the use of the simplified seeker model, simulation time can be reduced without the loss of simulation accuracy.
目的 研究风标头的动力学在制导航弹系统分析中的作用． 方法 对风标头的动力学进行分析，由于其时间常数很小，因此其动力学模型可大大简化． 结果与结论 在进行全弹的动力学仿真时，由于与弹体动力学相比风标头的时间常数很小，因此可采用其简化模型计算而不影响仿真的精度．
