• The result is satisfactory by using a method of the artificial earth satellite orbit determination from range rate observations to fit the free-flight trajectory of rocket.

    人造地球卫星轨道计算测速定轨方法拟合火箭飞行弹道的自由段,取得了比较满意结果

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  • By the study of extended range guided munitions (ERGM) trajectory characteristics, ERGM free-flight and glide trajectory characteristics are revealed and illustrated.

    研究揭示超远程炮弹无控段滑翔段的弹道特性

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  • By the study of extended range guided munitions (ERGM) trajectory characteristics, ERGM free-flight and glide trajectory characteristics are revealed and illustrated.

    研究揭示超远程炮弹无控段滑翔段的弹道特性

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