升力再入飞行器的混合模拟

A. Frederickson, R. B. Bailey, A. Saint-Paul
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引用次数: 1

摘要

在过去十年中,对各种类型的再入飞行器进行了大量的研究和开发工作。许多制导和控制再入飞行器的技术已经被提出。这次模拟的目的是评估一种新的再入飞行器飞行控制系统的能力,该系统本质上是简单、可靠和固有地确保安全再入的。随后的讨论解释了所研究的独特控制系统,并详细讨论了所需的仿真设备及其编程。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Hybrid simulation of a lifting re-entry vehicle
During the past ten years a great deal of research and development work has been conducted on various types of re-entry vehicles. Numerous techniques for guiding and controlling re-entry vehicles have been proposed. The purpose of this simulation is to evaluate the capability of a new flight control system for reentry vehicles which by its nature is simple, reliable and inherently insures a safe re-entry. The ensuing discussion explains the unique control system being studied, and includes a detailed discussion of the simulation equipment required and its programming.
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