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Missile Interceptor Integrated Guidance and Control: Single-Loop Higher-Order Sliding Mode Approach.

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	Missile Interceptor Integrated Guidance and Control: Single-Loop Higher-Order Sliding Mode Approach./
作者:	Cross, Michael.
出版者:	Ann Arbor : ProQuest Dissertations & Theses, : 2020,
面頁冊數:	156 p.
附註:	Source: Dissertations Abstracts International, Volume: 82-01, Section: B.
Contained By:	Dissertations Abstracts International82-01B.
標題:	Electrical engineering. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=27955838
ISBN:	9798662461192

Missile Interceptor Integrated Guidance and Control: Single-Loop Higher-Order Sliding Mode Approach.
Cross, Michael.

Missile Interceptor Integrated Guidance and Control: Single-Loop Higher-Order Sliding Mode Approach. - Ann Arbor : ProQuest Dissertations & Theses, 2020 - 156 p.

Source: Dissertations Abstracts International, Volume: 82-01, Section: B.

Thesis (Ph.D.)--The University of Alabama in Huntsville, 2020.

This item must not be sold to any third party vendors.

Traditionally, a missile interceptor's three-loop autopilot relies on every sensor to be working at all times for an intercept to occur. With faulty sensors and countermeasures becoming more sophisticated, sensor improvements alone may not be enough. In this research, an alternative structure is presented that does not rely on multiple sensors. Instead, it consists of a single-loop using only the relative normal velocity as feedback in an integrated guidance and control (IGC) structure. This establishes a direct link between the feedback and the missile's control surfaces. At its core, the IGC uses higher-order sliding mode control techniques to execute the intercept strategy. Three different higher-order integrated guidance and control algorithms are presented and compared through simulations to a traditional (G\\&C) system. Two of these are designed with only the knowledge of the input-output relative degree of the missile and the target's acceleration bounds. The third is an adaptive control strategy that only requires the input-output relative degree and instead adapts by estimating a lumped disturbance on the system. Each of these control algorithms were judged on performance and output signal smoothness as a means for determining their practicality in a real missile interceptor.

ISBN: 9798662461192Subjects--Topical Terms:

596380
Electrical engineering.
Subjects--Index Terms:

Control

Missile Interceptor Integrated Guidance and Control: Single-Loop Higher-Order Sliding Mode Approach.
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260 1 $a Ann Arbor : $b ProQuest Dissertations & Theses, $c 2020
300 $a 156 p.
500 $a Source: Dissertations Abstracts International, Volume: 82-01, Section: B.
500 $a Advisor: Shtessel, Yuri.
502 $a Thesis (Ph.D.)--The University of Alabama in Huntsville, 2020.
506 $a This item must not be sold to any third party vendors.
520 $a Traditionally, a missile interceptor's three-loop autopilot relies on every sensor to be working at all times for an intercept to occur. With faulty sensors and countermeasures becoming more sophisticated, sensor improvements alone may not be enough. In this research, an alternative structure is presented that does not rely on multiple sensors. Instead, it consists of a single-loop using only the relative normal velocity as feedback in an integrated guidance and control (IGC) structure. This establishes a direct link between the feedback and the missile's control surfaces. At its core, the IGC uses higher-order sliding mode control techniques to execute the intercept strategy. Three different higher-order integrated guidance and control algorithms are presented and compared through simulations to a traditional (G\\&C) system. Two of these are designed with only the knowledge of the input-output relative degree of the missile and the target's acceleration bounds. The third is an adaptive control strategy that only requires the input-output relative degree and instead adapts by estimating a lumped disturbance on the system. Each of these control algorithms were judged on performance and output signal smoothness as a means for determining their practicality in a real missile interceptor.
590 $a School code: 0278.
650 4 $a Electrical engineering. $3 596380
650 4 $a Aerospace engineering. $3 686400
653 $a Control
653 $a Guidance
653 $a Integrated guidance and control
653 $a Missile
653 $a Single-loop
653 $a Sliding mode control
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690 $a 0538
710 2 $a The University of Alabama in Huntsville. $b Electrical and Computer Engineering. $3 1182201
773 0 $t Dissertations Abstracts International $g 82-01B.
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792 $a 2020
793 $a English
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