| 弹道导弹轨迹发生器的设计 |
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| 引用本文： | 敖宏奎,王宏力,侯青剑,孙渊. 弹道导弹轨迹发生器的设计[J]. 兵工自动化, 2007, 26(8): 66-68 |
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| 作者姓名： | 敖宏奎 王宏力 侯青剑 孙渊 |
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| 作者单位： | 第二炮兵工程学院,303教研室,陕西,西安,710025;第二炮兵工程学院,303教研室,陕西,西安,710025;第二炮兵工程学院,303教研室,陕西,西安,710025;第二炮兵工程学院,303教研室,陕西,西安,710025 |
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| 摘 要： | 用于捷联惯导的弹道导弹轨迹发生器设计,包括动力学方程的建立和发射点惯性坐标系下的轨迹参数确定.后者又包含发射点惯性系下速度、位置、姿态角、比力速据及角速度的确定.针对误差公式推导复杂的特点,用导航仿真对其输出的角速率和比力值进行精度估计,验证了该设计的正确性.
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| 关 键 词： | 轨迹发生器 捷联惯导系统 仿真 |
| 文章编号： | 1006-1576（2007）08-0066-03 |
| 收稿时间： | 2007-06-25 |
| 修稿时间： | 2007-06-252007-07-18 |
Design of Ballistic Missile Trajectory Generator |
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| AO Hong-kui,WANG Hong-li,HOU Qing-jian,SUN Yuan. Design of Ballistic Missile Trajectory Generator[J]. Ordnance Industry Automation, 2007, 26(8): 66-68 |
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| Authors: | AO Hong-kui WANG Hong-li HOU Qing-jian SUN Yuan |
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| Abstract: | The design of a ballistic missile trajectory generator for SINS includes the establishing of dynamics equation and the confirming of trajectory parameter based on the launch inertial coordinates. The latter includes the confirming of velocity, position, attitude angle, the specific force and the angular velocity. For complex characteristics error formulas, the accuracy of its outputs, the specific force and the angular velocity are evaluated by using the method of SINS simulation. The results ,show that the design is successful. |
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| Keywords: | Trajectory generator Strap inertial navigation system (SINS) Simulation |
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