東華大學圖書館 |

Language: English

Help

回圖書館首頁

手機版館藏查詢

Back

Switch To: Labeled | MARC Mode | ISBD

A Design Concept for Launch and Reco...

Palmaccio, Brendan.

Linked to FindBook

Google Book

Amazon

博客來

A Design Concept for Launch and Recovery of REMUS 100 AUV from WAM-V 16 USV.

Record Type:	Electronic resources : Monograph/item
Title/Author:	A Design Concept for Launch and Recovery of REMUS 100 AUV from WAM-V 16 USV./
Author:	Palmaccio, Brendan.
Published:	Ann Arbor : ProQuest Dissertations & Theses, : 2023,
Description:	111 p.
Notes:	Source: Masters Abstracts International, Volume: 84-11.
Contained By:	Masters Abstracts International84-11.
Subject:	Ocean engineering. -
Online resource:	https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=30490180
ISBN:	9798379534882

A Design Concept for Launch and Recovery of REMUS 100 AUV from WAM-V 16 USV.
Palmaccio, Brendan.

A Design Concept for Launch and Recovery of REMUS 100 AUV from WAM-V 16 USV. - Ann Arbor : ProQuest Dissertations & Theses, 2023 - 111 p.

Source: Masters Abstracts International, Volume: 84-11.

Thesis (M.S.)--Florida Atlantic University, 2023.

In this thesis, feasibility of a concept for launch and recovery of the REMUS AUV from WAM-V USV is investigated. A modular recovery system which can be added to the WAM-V payload tray was designed, and based on a review of previous literature a CONOPS was developed for the launch and recovery process. The first phase of the CONOPS, which pertains to the position of the REMUS initially on the free surface prior to sling engagement is simulated using ANSYS AQWA. Preprocessing for the simulation involved simplification of the model in ANSYS SpaceClaim to achieve a proper mesh as well as theoretical calculations of the input parameters for wave environment and point masses etc. The simulation was evaluated by taking into consideration two wave environment scenarios: beam sea's (-90 degrees) and head seas (0 degrees). The wave environment was based on a linear frequency range for the waves which considered wavelengths that correspond to half and double the length of the WAM-V 16'. The significance of the simulation is characterized through identifying the ideal direction and wave frequency range for recovery based on the RAOs of the two vehicles.

ISBN: 9798379534882Subjects--Topical Terms:

660731
Ocean engineering.
Subjects--Index Terms:

Design concept

A Design Concept for Launch and Recovery of REMUS 100 AUV from WAM-V 16 USV.
LDR:02338nmm a2200409 4500 001 2402006
005 20241028114730.5
006 m o d
007 cr#unu||||||||
008 251215s2023 ||||||||||||||||| ||eng d
020 $a 9798379534882
035 $a (MiAaPQ)AAI30490180
035 $a AAI30490180
035 $a 2402006
040 $a MiAaPQ $c MiAaPQ
100 1 $a Palmaccio, Brendan. $0 (orcid)0009-0006-2569-6157 $3 3772222
245 1 2 $a A Design Concept for Launch and Recovery of REMUS 100 AUV from WAM-V 16 USV.
260 1 $a Ann Arbor : $b ProQuest Dissertations & Theses, $c 2023
300 $a 111 p.
500 $a Source: Masters Abstracts International, Volume: 84-11.
500 $a Advisor: Dhanak, Manhar.
502 $a Thesis (M.S.)--Florida Atlantic University, 2023.
520 $a In this thesis, feasibility of a concept for launch and recovery of the REMUS AUV from WAM-V USV is investigated. A modular recovery system which can be added to the WAM-V payload tray was designed, and based on a review of previous literature a CONOPS was developed for the launch and recovery process. The first phase of the CONOPS, which pertains to the position of the REMUS initially on the free surface prior to sling engagement is simulated using ANSYS AQWA. Preprocessing for the simulation involved simplification of the model in ANSYS SpaceClaim to achieve a proper mesh as well as theoretical calculations of the input parameters for wave environment and point masses etc. The simulation was evaluated by taking into consideration two wave environment scenarios: beam sea's (-90 degrees) and head seas (0 degrees). The wave environment was based on a linear frequency range for the waves which considered wavelengths that correspond to half and double the length of the WAM-V 16'. The significance of the simulation is characterized through identifying the ideal direction and wave frequency range for recovery based on the RAOs of the two vehicles.
590 $a School code: 0119.
650 4 $a Ocean engineering. $3 660731
650 4 $a Design. $3 518875
650 4 $a Naval engineering. $3 3173824
653 $a Design concept
653 $a Launch
653 $a Recovery
653 $a Modular recovery system
653 $a Wave environment
653 $a Linear frequency range
690 $a 0547
690 $a 0389
690 $a 0468
710 2 $a Florida Atlantic University. $b Ocean Engineering. $3 3173823
773 0 $t Masters Abstracts International $g 84-11.
790 $a 0119
791 $a M.S.
792 $a 2023
793 $a English
856 4 0 $u https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=30490180