一种新的方法来计算状态过渡矩阵,因为无香转换
Rahil Makadia1, Davide Farnocchia2, Steven R Chesley2
1Department of Aerospace Engineering, University of Illinois at Urbana-Champaign, 104 S. Wright St., Urbana, IL 61801 USA.
概括
我们为非线性动态系统开发了一种新的无气质转换方法. 这种方法通过避免衍生和任意步骤来简化计算,与传统的性能相匹配.
科学领域:
- 动态系统和控制理论.
- 天体动力学和太空飞行机械学
- 计算数学 计算数学 计算数学
背景情况:
- 状态过渡矩阵对于分析非线性动态系统至关重要.
- 像有限差异这样的传统方法涉及复杂的导数或任意的步骤大小.
- 在许多科学和工程应用中,准确地传播不确定性是必不可少的.
研究的目的:
- 引入一种新的,简化的方法来计算非线性动态系统的状态过渡矩阵.
- 消除了复杂的部分导数和任意扰动步骤的需要.
- 在各种应用中评估拟议方法的性能和准确性.
主要方法:
- 拟议的方法利用无味变换来计算状态过渡矩阵.
- 它避免了雅可比矩阵和自动区分的明确计算.
- 该方法在两体问题,火星大气入口和小行星近距离碰撞上进行了测试.
主要成果:
- 没有香味的转换状态过渡矩阵被证明可以保持简单性.
- 性能与经典的无气味转换方法相提并论.
- 这种新方法准确地复制了蒙特卡洛模拟的后面分布,即使具有刚性动态.
结论:
- 提出的无香转换方法为计算非线性系统中的状态过渡矩阵提供了一个强大的和简化的替代方案.
- 它保持了准确性和理想的特性,如简易性.
- 该方法在天体动力学,飞行力学和其他涉及复杂动力学的领域具有广泛的适用性.
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