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zi you fei xing duan fen xi fang fa
Author(s): WU Liren
Pages: 8-
12
Year: 1987
Issue:
3
Journal: Aerospace Control
Keyword: 制导误差; 精度分析; 自由飞行轨迹;
Abstract: 本文介绍导弹飞行试验时,用雷达或光测设备在自由飞行段进行跟踪,应用最小二乘法原理,对离散测量数据进行处理,以确定飞行器轨道参数的最佳线性化估值方法。这种方法对评定导弹的精度是行之有效的。并适用于其它飞行器的测轨问题。
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