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hang tian kong zhi 1987 nian fen lei mu lu
Pages: 59-60
Year: Issue:  4
Journal: Aerospace Control

Keyword:  分类目录惯性制导激光陀螺固体火箭发动机抗电磁脉冲导弹测试陀螺罗盘广播卫星最优控制问题极大值原理;
Abstract: 快速傅里叶变换(FFT)在导弹测试系统中的应用 “..............……“······……包为民孙永成范金瑜地地战术导弹全程惯性制导巾陀螺误差的}』补偿·············“··一王枚之二阶组合测高环节的分析与设计·“···”·····,··“·”“···········”……张佑忠感应同步器位置侧量系统的正交误差及补偿·········”…于锡武孟宪华固体火箭发动机瞬态推力侧试装置················”···..····“·····”…楼靖波用极大值原理使航天飞机的降落弹道最佳化“··““·“.···”······一王永平自由飞行段分析方法············
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