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Learn-to-fly Control System Design.

Old Dominion University.

Learn-to-fly Control System Design.

紀錄類型:	書目-語言資料,手稿 : Monograph/item
正題名/作者:	Learn-to-fly Control System Design./
作者:	Streit, Alexander Brent.
面頁冊數:	1 online resource (56 pages)
附註:	Source: Masters Abstracts International, Volume: 57-06.
Contained By:	Masters Abstracts International57-06(E).
標題:	Electrical engineering. -
電子資源:	click for full text (PQDT)
ISBN:	9780438022126

Learn-to-fly Control System Design.
Streit, Alexander Brent.

Learn-to-fly Control System Design. - 1 online resource (56 pages)

Source: Masters Abstracts International, Volume: 57-06.

Thesis (M.S.)--Old Dominion University, 2018.

Includes bibliographical references

In order to improve aircraft flight control system development life cycle, new flight control techniques are being explored to allow the system to "learn-to-fly" with limited a priori information of the aircraft's aerodynamic characteristics. One approach is to have a system identification process operating on-the-fly to generate mathematical models which can be used to update control laws. In this thesis, a wind tunnel experiment was conducted with a model aircraft set up to be free-to-roll, so system identification and control methods could be explored for a one-degree-of-freedom case. In particular this thesis covers the design of a novel control system that uses mathematical models of a predetermined form with certain unknown parameters to achieve satisfactory roll control for the free-to-roll experiment. The mathematical model was updated on-the-fly by a separate process that is outside of the scope of this thesis, which performs system identification in real-time.

Electronic reproduction.
Ann Arbor, Mich. :
ProQuest,
2018

Mode of access: World Wide Web

ISBN: 9780438022126Subjects--Topical Terms:

596380
Electrical engineering.
Index Terms--Genre/Form:

554714
Electronic books.

Learn-to-fly Control System Design.
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100 1 $a Streit, Alexander Brent. $3 1194282
245 1 0 $a Learn-to-fly Control System Design.
264 0 $c 2018
300 $a 1 online resource (56 pages)
336 $a text $b txt $2 rdacontent
337 $a computer $b c $2 rdamedia
338 $a online resource $b cr $2 rdacarrier
500 $a Source: Masters Abstracts International, Volume: 57-06.
500 $a Adviser: Oscar R. Gonzalez.
502 $a Thesis (M.S.)--Old Dominion University, 2018.
504 $a Includes bibliographical references
520 $a In order to improve aircraft flight control system development life cycle, new flight control techniques are being explored to allow the system to "learn-to-fly" with limited a priori information of the aircraft's aerodynamic characteristics. One approach is to have a system identification process operating on-the-fly to generate mathematical models which can be used to update control laws. In this thesis, a wind tunnel experiment was conducted with a model aircraft set up to be free-to-roll, so system identification and control methods could be explored for a one-degree-of-freedom case. In particular this thesis covers the design of a novel control system that uses mathematical models of a predetermined form with certain unknown parameters to achieve satisfactory roll control for the free-to-roll experiment. The mathematical model was updated on-the-fly by a separate process that is outside of the scope of this thesis, which performs system identification in real-time.
533 $a Electronic reproduction. $b Ann Arbor, Mich. : $c ProQuest, $d 2018
538 $a Mode of access: World Wide Web
650 4 $a Electrical engineering. $3 596380
650 4 $a Aerospace engineering. $3 686400
655 7 $a Electronic books. $2 local $3 554714
690 $a 0544
690 $a 0538
710 2 $a ProQuest Information and Learning Co. $3 1178819
710 2 $a Old Dominion University. $b Electrical/Computer Engineering. $3 1191987
773 0 $t Masters Abstracts International $g 57-06(E).
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=10813121 $z click for full text (PQDT)

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