Safety analysis of TCAS on Global Hawk using airspace encounter models

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006.

Bibliographic Details
Main Author: Billingsley, Thomas B. (Thomas Boyd)
Other Authors: James K. Kuchar and Jonathan P. How.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2007
Subjects:
Online Access:http://hdl.handle.net/1721.1/35294
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author Billingsley, Thomas B. (Thomas Boyd)
author2 James K. Kuchar and Jonathan P. How.
author_facet James K. Kuchar and Jonathan P. How.
Billingsley, Thomas B. (Thomas Boyd)
author_sort Billingsley, Thomas B. (Thomas Boyd)
collection MIT
description Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006.
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spelling mit-1721.1/352942019-04-12T14:44:05Z Safety analysis of TCAS on Global Hawk using airspace encounter models Safety analysis of Traffic Alert and Collision Avoidance System on Global Hawk using airspace encounter models Billingsley, Thomas B. (Thomas Boyd) James K. Kuchar and Jonathan P. How. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006. This electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections. Includes bibliographical references (p. 66). The U.S. Air Force's RQ-4 Global Hawk unmanned aerial vehicle (UAV) is a high altitude, long endurance aircraft used for surveillance and reconnaissance. Because of the potential for close proximity to manned aircraft in civil airspace, collision avoidance is a major concern, and the Air Force is seeking to equip Global Hawk with the Traffic Alert and Collision Avoidance System (TCAS) to reduce the probability of mid-air collision. Currently, Global Hawk is equipped with a Mode S transponder and uses chase aircraft, ground observers and/or ground radar contact to comply with the collision avoidance requirement. In order to evaluate TCAS effectiveness, a fast-time simulation tool has been developed at MIT Lincoln Laboratory that computes the mean probability of a near mid-air collision for a large number of close encounters between two aircraft. Airspace encounter models enable sets of encounters to be simulated that are statistically representative of the aircraft encounters that actually occur in the airspace. The TCAS logic is implemented in the simulation tool and the aircraft responses during the encounters, with and without TCAS, are simulated in parallel. (cont.) By observing measured vertical miss distance at the closest point of approach between the two aircraft, it is possible to quantify the reduction in collision risk provided by TCAS, termed the risk ratio. Global Hawk's flight characteristics differ from a conventional aircraft. Its mission profile through civil airspace includes slow, steep climbs and descents, and shallower turns than a conventional aircraft. Its vertical acceleration and climb rate limits can hinder its response to a TCAS resolution advisory (RA). Communication latency also may occur. For this thesis, encounter models were developed that reflect Global Hawk's flight characteristics. The new encounter models were then implemented in the simulation tool, and millions of encounters between Global Hawk and a conventional aircraft were simulated. These encounters were compared against encounters between two conventional aircraft to observe how Global Hawk's flight characteristics changed the effectiveness of TCAS. Assuming a standard pilot response to TCAS RAs, TCAS provided a significant safety improvement to Global Hawk over a Mode S transponder alone, yielding risk ratios in the range of 0.003 to 0.079. (cont.) Global Hawk's flight characteristics generally caused a decrease in TCAS effectiveness from the original encounter models. Encounters were also simulated where Global Hawk's response to TCAS RAs was delayed by increasing amounts to simulate communication latency. A delay of approximately 15 seconds was tolerable before TCAS provided less safety than a Mode S transponder alone. by Thomas B. Billingsley. S.M. 2007-01-10T15:35:50Z 2007-01-10T15:35:50Z 2006 2006 Thesis http://hdl.handle.net/1721.1/35294 74468299 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 66 p. 2077489 bytes 2084658 bytes application/pdf application/pdf application/pdf Massachusetts Institute of Technology
spellingShingle Aeronautics and Astronautics.
Billingsley, Thomas B. (Thomas Boyd)
Safety analysis of TCAS on Global Hawk using airspace encounter models
title Safety analysis of TCAS on Global Hawk using airspace encounter models
title_full Safety analysis of TCAS on Global Hawk using airspace encounter models
title_fullStr Safety analysis of TCAS on Global Hawk using airspace encounter models
title_full_unstemmed Safety analysis of TCAS on Global Hawk using airspace encounter models
title_short Safety analysis of TCAS on Global Hawk using airspace encounter models
title_sort safety analysis of tcas on global hawk using airspace encounter models
topic Aeronautics and Astronautics.
url http://hdl.handle.net/1721.1/35294
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