Test and Evaluation of the Piccolo Autopilot System on a One-Third Scale Yak-54

To gain a better understanding of the dynamics of the great ice sheets the National Science Foundation established the Center for Remote Sensing of Ice Sheets (CReSIS) to develop technologies that would improve data gathering of said ice sheets. CReSIS was tasked with the development of an unmanned...

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Main Author: Jager, Rylan Walter
Other Authors: Downing, David, Colgren, Richard, Hale, Richard
Format: Thesis
Language:English
Published: University of Kansas 2008
Subjects:
Online Access:http://hdl.handle.net/1808/3997
http://dissertations.umi.com/ku:2513
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author Jager, Rylan Walter
author2 Downing, David
Colgren, Richard
Hale, Richard
author_facet Jager, Rylan Walter
author_sort Jager, Rylan Walter
collection The University of Kansas: KU ScholarWorks
description To gain a better understanding of the dynamics of the great ice sheets the National Science Foundation established the Center for Remote Sensing of Ice Sheets (CReSIS) to develop technologies that would improve data gathering of said ice sheets. CReSIS was tasked with the development of an unmanned aerial vehicle, named the Meridian, which would have the ability to make use of advanced radar systems that could be used to gather data on the ice sheets of remote Polar Regions. CReSIS decided to use commercial-off-the-shelf autopilot systems on the Meridian, selecting the Cloud Cap Technologies Piccolo II UAV autopilot system as the initial system to be tested and evaluated. A process for test and evaluation of modeling, simulation and control systems is presented. Three dynamic models for a one-third scale Yak-54 are developed. A deliberate and methodical flight test program is developed to evaluate the Piccolo II flight control system. Parameter identification flight tests are performed to evaluate the three modeling and simulation techniques. Closed loop flight testing is performed to evaluate the flight control system's ability to control an aircraft and the ability of the gains to be performance optimized. Finally flaws are found in the communication system architecture of the Piccolo II autopilot system which causes the system to go pilot-in-loop unstable and to be rejected from further consideration by the CReSIS team.
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genre Center for Remote Sensing of Ice Sheets (CReSIS)
genre_facet Center for Remote Sensing of Ice Sheets (CReSIS)
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op_rights This item is protected by copyright and unless otherwise specified the copyright of this thesis/dissertation is held by the author.
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spelling ftunivkansas:oai:kuscholarworks.ku.edu:1808/3997 2025-01-16T21:29:16+00:00 Test and Evaluation of the Piccolo Autopilot System on a One-Third Scale Yak-54 Jager, Rylan Walter Downing, David Colgren, Richard Hale, Richard 2008 208 pages http://hdl.handle.net/1808/3997 http://dissertations.umi.com/ku:2513 EN eng University of Kansas http://dissertations.umi.com/ku:2513 http://hdl.handle.net/1808/3997 This item is protected by copyright and unless otherwise specified the copyright of this thesis/dissertation is held by the author. openAccess Aerospace engineering Thesis 2008 ftunivkansas 2022-08-26T13:09:21Z To gain a better understanding of the dynamics of the great ice sheets the National Science Foundation established the Center for Remote Sensing of Ice Sheets (CReSIS) to develop technologies that would improve data gathering of said ice sheets. CReSIS was tasked with the development of an unmanned aerial vehicle, named the Meridian, which would have the ability to make use of advanced radar systems that could be used to gather data on the ice sheets of remote Polar Regions. CReSIS decided to use commercial-off-the-shelf autopilot systems on the Meridian, selecting the Cloud Cap Technologies Piccolo II UAV autopilot system as the initial system to be tested and evaluated. A process for test and evaluation of modeling, simulation and control systems is presented. Three dynamic models for a one-third scale Yak-54 are developed. A deliberate and methodical flight test program is developed to evaluate the Piccolo II flight control system. Parameter identification flight tests are performed to evaluate the three modeling and simulation techniques. Closed loop flight testing is performed to evaluate the flight control system's ability to control an aircraft and the ability of the gains to be performance optimized. Finally flaws are found in the communication system architecture of the Piccolo II autopilot system which causes the system to go pilot-in-loop unstable and to be rejected from further consideration by the CReSIS team. Thesis Center for Remote Sensing of Ice Sheets (CReSIS) The University of Kansas: KU ScholarWorks
spellingShingle Aerospace engineering
Jager, Rylan Walter
Test and Evaluation of the Piccolo Autopilot System on a One-Third Scale Yak-54
title Test and Evaluation of the Piccolo Autopilot System on a One-Third Scale Yak-54
title_full Test and Evaluation of the Piccolo Autopilot System on a One-Third Scale Yak-54
title_fullStr Test and Evaluation of the Piccolo Autopilot System on a One-Third Scale Yak-54
title_full_unstemmed Test and Evaluation of the Piccolo Autopilot System on a One-Third Scale Yak-54
title_short Test and Evaluation of the Piccolo Autopilot System on a One-Third Scale Yak-54
title_sort test and evaluation of the piccolo autopilot system on a one-third scale yak-54
topic Aerospace engineering
topic_facet Aerospace engineering
url http://hdl.handle.net/1808/3997
http://dissertations.umi.com/ku:2513