High-Speed Aircraft Stability and Control Metrics

This review paper identifies key stability and control screening parameters needed to design low-risk, general-purpose high-speed aircraft. These derive from MIL-STD-8785C, MIL-STD-1797, and older AGARD reports, and are suitable for assessing conceptual high-speed vehicles. We demonstrate their appl...

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Main Authors: Timothy T. Takahashi, Jack A. Griffin, Ramana V. Grandhi
Format: Article
Language:English
Published: MDPI AG 2024-12-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/12/1/12
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author Timothy T. Takahashi
Jack A. Griffin
Ramana V. Grandhi
author_facet Timothy T. Takahashi
Jack A. Griffin
Ramana V. Grandhi
author_sort Timothy T. Takahashi
collection DOAJ
description This review paper identifies key stability and control screening parameters needed to design low-risk, general-purpose high-speed aircraft. These derive from MIL-STD-8785C, MIL-STD-1797, and older AGARD reports, and are suitable for assessing conceptual high-speed vehicles. We demonstrate their applicability using published ground test, computation, and flight test data from the Bell X-2, North American X-15, Martin X-24A, Northrop HL-10, Lockheed Blackbird (YF-12/SR-71), and North American XB-70 as well as the Rockwell Space Shuttle Orbiter. The relative success of the X-15 and Blackbird and the performance limitations of the others indicate the need to scrutinize lateral-directional stability at the preliminary design phase. Our work reveals the need for strong bare-airframe static directional stability to obtain favorable flying qualities.
format Article
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institution Kabale University
issn 2226-4310
language English
publishDate 2024-12-01
publisher MDPI AG
record_format Article
series Aerospace
spelling doaj-art-acbde03e163d4bb4ad41244274718ed32025-01-24T13:15:26ZengMDPI AGAerospace2226-43102024-12-011211210.3390/aerospace12010012High-Speed Aircraft Stability and Control MetricsTimothy T. Takahashi0Jack A. Griffin1Ramana V. Grandhi2Air Force Institute of Technology, Wright Patterson Air Force Base, Dayton, OH 45433, USAAir Force Institute of Technology, Wright Patterson Air Force Base, Dayton, OH 45433, USAAir Force Institute of Technology, Wright Patterson Air Force Base, Dayton, OH 45433, USAThis review paper identifies key stability and control screening parameters needed to design low-risk, general-purpose high-speed aircraft. These derive from MIL-STD-8785C, MIL-STD-1797, and older AGARD reports, and are suitable for assessing conceptual high-speed vehicles. We demonstrate their applicability using published ground test, computation, and flight test data from the Bell X-2, North American X-15, Martin X-24A, Northrop HL-10, Lockheed Blackbird (YF-12/SR-71), and North American XB-70 as well as the Rockwell Space Shuttle Orbiter. The relative success of the X-15 and Blackbird and the performance limitations of the others indicate the need to scrutinize lateral-directional stability at the preliminary design phase. Our work reveals the need for strong bare-airframe static directional stability to obtain favorable flying qualities.https://www.mdpi.com/2226-4310/12/1/12flight dynamicssupersonichypersonicflying qualitiesstabilitycontrol
spellingShingle Timothy T. Takahashi
Jack A. Griffin
Ramana V. Grandhi
High-Speed Aircraft Stability and Control Metrics
Aerospace
flight dynamics
supersonic
hypersonic
flying qualities
stability
control
title High-Speed Aircraft Stability and Control Metrics
title_full High-Speed Aircraft Stability and Control Metrics
title_fullStr High-Speed Aircraft Stability and Control Metrics
title_full_unstemmed High-Speed Aircraft Stability and Control Metrics
title_short High-Speed Aircraft Stability and Control Metrics
title_sort high speed aircraft stability and control metrics
topic flight dynamics
supersonic
hypersonic
flying qualities
stability
control
url https://www.mdpi.com/2226-4310/12/1/12
work_keys_str_mv AT timothyttakahashi highspeedaircraftstabilityandcontrolmetrics
AT jackagriffin highspeedaircraftstabilityandcontrolmetrics
AT ramanavgrandhi highspeedaircraftstabilityandcontrolmetrics