通过使用双轴旋转惯性导航系统的模式切换策略来提高发射车的轨道注射精度
Jun Li1,2, Shifeng Zhang1,2, Zhenlin Ma1,2
1College of Aerospace and Engineering, National University of Defense Technology, Changsha 410073, China.
Sensors (Basel, Switzerland)
|January 11, 2025
概括
一个新的模式切换策略提高了发射车轨道注入精度. 通过利用近平台和带下模式,这种方法可提高12-13%的精度,成本增加最小.
科学领域:
- 航空航天工程 航空航天工程
- 导航系统 导航系统
- 导航,导航和控制是指导,导航和控制.
背景情况:
- 发射车中的双轴旋转惯性导航系统由于飞行时间短,往往未得到充分利用.
- 目前的系统通常以紧固式模式运行,无法充分利用旋转调制的全部精度潜力.
研究的目的:
- 提出和评估一种模式切换策略,以提高发射车的轨道注射精度.
- 为了优化旋转惯性导航系统的使用,通过在近平台和紧带式模式之间切换.
主要方法:
- 在发射器飞行过程中实施旋转惯性导航系统的模式切换策略.
- 使用数值模拟和转盘实验来验证拟议的策略.
主要成果:
- 模式切换策略显著提高了轨道注射精度,相比传统的紧式模式.
- 实现了轨道精度的提高,从12%到13%不等.
结论:
- 拟议的模式切换策略有效地提高了发射车轨道注入精度.
- 这种方法提供了一种具有成本效益的解决方案,可以提高导航精度,而无需增加大量费用.
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