Skip to main content
Communities & Collections
All of DSpace
Statistics
English
العربية
বাংলা
Català
Čeština
Deutsch
Ελληνικά
Español
Suomi
Français
Gàidhlig
हिंदी
Magyar
Italiano
Қазақ
Latviešu
Nederlands
Polski
Português
Português do Brasil
Srpski (lat)
Српски
Svenska
Türkçe
Yкраї́нська
Tiếng Việt
Log In
Log in
New user? Click here to register.
Have you forgotten your password?
Home
科技與工程學院
電機工程學系
學位論文
學位論文
Permanent URI for this collection
http://rportal.lib.ntnu.edu.tw/handle/20.500.12235/73890
Browse
Search
By Issue Date
By Author
By Title
By Subject
By Subject Category
Search
By Issue Date
By Author
By Title
By Subject
By Subject Category
1 results
Back to results
Filters
Author
1
search.filters.author.Wu, Chi-Hsun
1
search.filters.author.吳祈勳
Subject
search.filters.subject.cascade fuzzy PID controller
1
search.filters.subject.altitude control
1
search.filters.subject.attitude control
1
search.filters.subject.Quadcopter
1
search.filters.subject.串級模糊PID控制器
Show more
Search subject
Submit
Browse subject tree
Date
Start
End
Submit
2021
1
Has files
1
No
Reset filters
Settings
Sort By
Accessioned Date Descending
Most Relevant
Title Ascending
Date Issued Descending
Results per page
1
5
10
20
40
60
80
100
Search
Subject: search.filters.subject.cascade fuzzy PID controller
×
Search Tools
Search Results
Now showing
1 - 1 of 1
No Thumbnail Available
Item
四旋翼無人機之模糊PID控制器設計與實現
(
2021
)
吳祈勳
;
Wu, Chi-Hsun
Show more
本論文設計了一套四旋翼飛行器系統,利用串級模糊 PID (Proportional–Integral–Derivative)控制器,來完成俯仰角(Pitch)、翻滾角(Roll)、偏航角(Yaw)與高度(altitude)的定位控制。並在文中探討各項因素對飛行器整體所造成的影響。一般商業四旋翼飛行器所採用的控制器常使用串級PID控制器,其優點就是面對飛行器這種複雜的非線性系統,不需要透過建立精確數學模型,依然能有效控制。但定值的PID參數在面對各種突發情況下,並非是當下最合適的值。為了能在不同的情況下,提供適當PID增益參數,因此導入模糊理論至PID控制器,形成串級式模糊 PID控制器。透過不同控制器間的相互比較來證實此方法的可行性,並會對各增益參數與模糊規則進行探討。最後,透過許多實驗設計,來測試本論文所提四旋翼飛行器的性能。
Show more