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Constraint Force Equation Methodology for Modeling Multi-Body Stage Separation Dynamics

机译:建模多主体分离动力学的约束力方程方法

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摘要

This paper discusses a generalized approach to the multi-body separation problems in a launch vehicle staging environment based on constraint force methodology and its implementation into the Program to Optimize Simulated Trajectories II (POST2), a widely used trajectory design and optimization tool. This development facilitates the inclusion of stage separation analysis into POST2 for seamless end-to-end simulations of launch vehicle trajectories, thus simplifying the overall implementation and providing a range of modeling and optimization capabilities that are standard features in POST2. Analysis and results are presented for two test cases that validate the constraint force equation methodology in a stand-alone mode and its implementation in POST2.
机译:本文讨论了一种基于约束力方法的运载火箭分级环境中多体分离问题的通用方法,并将其应用于广泛使用的轨迹设计和优化工具“优化仿真轨迹II”(POST2)中。此开发有助于将阶段分离分析包含到POST2中,以便对运载火箭的轨迹进行无缝的端到端仿真,从而简化了总体实现,并提供了一系列建模和优化功能,这些功能是POST2的标准功能。给出了两个测试案例的分析和结果,这两个测试案例以独立模式验证了约束力方程方法并在POST2中实现了该方法。

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