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Development of the Reentry Flight Dynamics Simulator for Evaluation of Space Shuttle Orbiter Entry Systems.

机译：用于评估航天飞机轨道器进入系统的再入飞行动力学模拟器的研制。

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摘要

A nonlinear, six degree of freedom, digital computer simulation of a vehicle which has constant mass properties and whose attitudes are controlled by both aerodynamic surfaces and reaction control system thrusters was developed. A rotating, oblate Earth model was used to describe the gravitational forces which affect long duration Earth entry trajectories. The program is executed in a nonreal time mode or connected to a simulation cockpit to conduct piloted and autopilot studies. The program guidance and control software used by the space shuttle orbiter for its descent from approximately 121.9 km to touchdown on the runway.

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作者
rowell, l. f. powell, r. w.;
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年度 1980
页码 1-97
总页数 97
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Computerized simulation; Digital computers; Onboard equipment; Reentry guidance; Space shuttle orbiters; Spacecraft reentry; Automatic pilots; Computer programs; Digital simulation; Mathematical models; Recoverable spacecraft; Reusable spacecraft;

机译：计算机模拟;数字计算机;车载设备;再入制导;航天飞机轨道飞行器;航天器再入;自动驾驶仪;计算机程序;数字仿真;数学模型;可回收航天器;可重复使用的航天器;

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专利

1. Unmanned X-37B orbital test vehicle begins second flight--Crewless spacecraft could replace Space Shuttle and reduce costs [J] . High-Performance Composites . 2011,第3期

机译：无人X-37B轨道测试飞行器开始第二次飞行-无人驾驶的航天器可以取代航天飞机并降低成本
2. Implementation of an Aerodynamic Toolbox in a Reentry Flight Simulator [J] . A. Guidi, Q. P. Chu, J. A. Mulder, Journal of Spacecraft and Rockets . 2003,第1期

机译：再入飞行模拟器中气动工具箱的实现
3. Robust optimal onboard reentry guidance of a space shuttle: Dynamic game approach and guidance synthesis via neural networks [J] . Breitner MH. Journal of Optimization Theory and Applications . 2000,第3期

机译：航天飞机的稳健最优入场重返制导：动态博弈方法和神经网络制导综合
4. External Computational Aerothermodynamic Anaysis of the Space Shuttle Orbiter at STS- 107 Flight Conditions [C] . J. Reuther, R. McDaniel, J. Brown, 34th AIAA Fluid Dynamics Conference ; 2nd AIAA Flow Control Conference ; 35th AIAA Plasmadynamics and Lasers Conference ; 37th AIAA Thermophysics Conference . 2004

机译：STS-107飞行条件下航天飞机轨道飞行器的外部计算空气热力学分析
5. ANALYSIS OF AERODYNAMIC PHENOMENA ASSOCIATED WITH THE QUARTZ-HERTZ MOTIONOF THE SPACE SHUTTLE ORBITER. [D] . BRANNAN, RAYMOND EUGENE, JR. 1987

机译：与航天飞机绕壁摆锤的石英-赫兹运动有关的气动现象分析。
6. Neurovestibular Considerations for Sub-Orbital Space Flight: A Framework for Future Investigation [O] . Faisal Karmali, Mark Shelhamer -1

机译：一个框架未来研究：对亚轨道太空飞行Neurovestibular注意事项
7. Evaluation of potential changes to the Space Shuttle Orbiter's Flight Control System to increase directional control during post landing rollout [O] . Ham Linda J. 1997

机译：评估航天飞机轨道飞行器的飞行控制系统的潜在变化，以在降落后发射期间增加方向控制
8. Development of the reentry flight dynamics simulator for evaluation of space shuttle orbiter entry systems [R] . Rowell, L. F., Powell, R. W., Stone, H. W., Jr. 1980

机译：开发用于评估航天飞机轨道器入口系统的再入飞行动力学模拟器

Development of the Reentry Flight Dynamics Simulator for Evaluation of Space Shuttle Orbiter Entry Systems.

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