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

Modeling, Controlling, and Simulatin...

Reed, Seth,

Linked to FindBook

Google Book

Amazon

博客來

Modeling, Controlling, and Simulating a Nose-Sitting Vertical Take-Off and Landing Aircraft /

Record Type:	Electronic resources : Monograph/item
Title/Author:	Modeling, Controlling, and Simulating a Nose-Sitting Vertical Take-Off and Landing Aircraft // Seth Reed.
Author:	Reed, Seth,
Description:	1 electronic resource (99 pages)
Notes:	Source: Masters Abstracts International, Volume: 86-01.
Contained By:	Masters Abstracts International86-01.
Subject:	Aerospace engineering. -
Online resource:	https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=31302281
ISBN:	9798383226964

Modeling, Controlling, and Simulating a Nose-Sitting Vertical Take-Off and Landing Aircraft /
Reed, Seth,

Modeling, Controlling, and Simulating a Nose-Sitting Vertical Take-Off and Landing Aircraft /Seth Reed. - 1 electronic resource (99 pages)

Source: Masters Abstracts International, Volume: 86-01.

The increasing frequency and severity of wildfires have created a pressing need for more e↵ective aerial firefighting solutions. An innovative nose-sitting vertical take-off and landing (VTOL) aircraft aims to address shortfalls of current drones used in wildfire missions. This research focused on developing a custom aircraft simulator, and on designing a basic autopilot control system for the aircraft's helicopter mode. Standard airplane simulation literature was referenced to produce the baseline aircraft model, but additional derivations were required to describe the propulsion system which uses a nested four-bar mechanism for thrust vectoring. Linear control systems for attitude, position, and altitude were designed using the method of successive loop closure. The controllers were implemented on the full 6DOF aircraft model, and tests were conducted to analyze the response to different orientation, position, and velocity commands. The results demonstrated that the autopilot control system effectively maintained stability and performance throughout each simulation. These findings lay the groundwork for future research and ultimately underscore the potential of nose-sitting VTOL aircraft to revolutionize aerial firefighting operations.

English

ISBN: 9798383226964Subjects--Topical Terms:

1002622
Aerospace engineering.
Subjects--Index Terms:

Autonomous control

Modeling, Controlling, and Simulating a Nose-Sitting Vertical Take-Off and Landing Aircraft /
LDR:02684nmm a22004333i 4500 001 2438596
005 20260727134359.5
006 m o d
007 cr|nu||||||||
008 261011s2024 miu||||||m |||||||eng d
020 $a 9798383226964
035 $a (MiAaPQD)AAI31302281
035 $a AAI31302281
040 $a MiAaPQD $b eng $c MiAaPQD $e rda
100 1 $a Reed, Seth, $e author. $3 3829955
245 1 0 $a Modeling, Controlling, and Simulating a Nose-Sitting Vertical Take-Off and Landing Aircraft / $c Seth Reed.
264 1 $a Ann Arbor : $b ProQuest Dissertations & Theses, $c 2024
300 $a 1 electronic resource (99 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: 86-01.
500 $a Advisors: Mesbahi, Mehran Committee members: Taghvaei, Amir.
502 $b M.S. $c University of Washington $d 2024.
520 $a The increasing frequency and severity of wildfires have created a pressing need for more e↵ective aerial firefighting solutions. An innovative nose-sitting vertical take-off and landing (VTOL) aircraft aims to address shortfalls of current drones used in wildfire missions. This research focused on developing a custom aircraft simulator, and on designing a basic autopilot control system for the aircraft's helicopter mode. Standard airplane simulation literature was referenced to produce the baseline aircraft model, but additional derivations were required to describe the propulsion system which uses a nested four-bar mechanism for thrust vectoring. Linear control systems for attitude, position, and altitude were designed using the method of successive loop closure. The controllers were implemented on the full 6DOF aircraft model, and tests were conducted to analyze the response to different orientation, position, and velocity commands. The results demonstrated that the autopilot control system effectively maintained stability and performance throughout each simulation. These findings lay the groundwork for future research and ultimately underscore the potential of nose-sitting VTOL aircraft to revolutionize aerial firefighting operations.
546 $a English
590 $a School code: 0250
650 4 $a Aerospace engineering. $3 1002622
650 4 $a Engineering. $3 586835
650 4 $a Aeronomy. $3 2102064
653 $a Autonomous control
653 $a Contra-rotating propellers
653 $a Nose sitting aircraft
653 $a Proportional control strategy
653 $a Thrust vectoring
690 $a 0538
690 $a 0367
690 $a 0537
710 2 $a University of Washington. $b Aeronautics and Astronautics. $e degree granting institution. $3 3829956
720 1 $a Mesbahi, Mehran $e degree supervisor.
773 0 $t Masters Abstracts International $g 86-01.
790 $a 0250
791 $a M.S.
792 $a 2024
856 4 0 $u https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=31302281