所确定的指标明显低于常见的空-空弹点源信号导引头的最大跟踪角速度。
The result is obviously lower than the maximum tracking speeds of point signal seekers of ordinary air to air missiles.
通过结合目标红外特征，研究了空-空弹在复杂背景条件下的目标红外成像末制导的技术原理和实施途径。
This paper, in connection with ir target signature research, deals with the principle and realization for the ir imaging terminal-guidance technology of air-to-air missile in clutter background.
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