東華大學圖書館 |

語系: 繁體中文

說明(常見問題)

回圖書館首頁

手機版館藏查詢

登入

回首頁 到查詢結果 [ null ]

切換: 標籤 | MARC模式 | ISBD

Considerations for Air Data Sensing ...

Oklahoma State University., Mechanical & Aerospace Engineering.

FindBook

Google Book

Amazon

博客來

Considerations for Air Data Sensing in Small UAS.

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Considerations for Air Data Sensing in Small UAS./
作者:	Sandwell, Jeffrey Allen.
出版者:	Ann Arbor : ProQuest Dissertations & Theses, : 2023,
面頁冊數:	67 p.
附註:	Source: Masters Abstracts International, Volume: 85-07.
Contained By:	Masters Abstracts International85-07.
標題:	Aerospace engineering. -
電子資源:	https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=30575871
ISBN:	9798381290257

Considerations for Air Data Sensing in Small UAS.
Sandwell, Jeffrey Allen.

Considerations for Air Data Sensing in Small UAS. - Ann Arbor : ProQuest Dissertations & Theses, 2023 - 67 p.

Source: Masters Abstracts International, Volume: 85-07.

Thesis (M.S.)--Oklahoma State University, 2023.

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

Modern unmanned aircraft in both the research and hobby fields often rely on hobby grade sensors for detection of airspeed and differential pressures. These sensors are used by both pilots and autopilot systems for control of the airframe, however the limits of these systems and their implementations are often not adequately understood. A full wind tunnel calibration of airframes with installed sensors would greatly reduce the errors before flight, but this is often not feasible due to size of aircraft or available facilities. This leaves most error correction to be done by flight testing which requires the risking of the airframe with potentially poor calibration values. Proper analysis of expected errors from probe type and placement are necessary to mitigate the risks to airspeed dependent airframes before they are able to gather the appropriate flight data for airspeed corrections. In addition to the standard error correction, a proper uncertainty analysis should be performed for all used sensors to ensure the feasibility of the measurements they are trying to obtain. This combination of analyses can be used to provide guidance for obtaining an airspeed measurement as well as other potential air data values. Angle of attack measurement is rarely available on small UAS systems, likely due to installation issues and lack of sensor accuracy over broad speed ranges. Similar to airspeed, general guidance and feasibility studies can be performed using expected errors and uncertainty analysis to determine the potential for using common airspeed sensors for the detection of an airframe's angle of attack.

ISBN: 9798381290257Subjects--Topical Terms:

1002622
Aerospace engineering.
Subjects--Index Terms:

Aircraft

Considerations for Air Data Sensing in Small UAS.
LDR:02827nmm a2200397 4500 001 2397255
005 20240617111357.5
006 m o d
007 cr#unu||||||||
008 251215s2023 ||||||||||||||||| ||eng d
020 $a 9798381290257
035 $a (MiAaPQ)AAI30575871
035 $a AAI30575871
040 $a MiAaPQ $c MiAaPQ
100 1 $a Sandwell, Jeffrey Allen. $3 3767018
245 1 0 $a Considerations for Air Data Sensing in Small UAS.
260 1 $a Ann Arbor : $b ProQuest Dissertations & Theses, $c 2023
300 $a 67 p.
500 $a Source: Masters Abstracts International, Volume: 85-07.
500 $a Advisor: Arena, Andy.
502 $a Thesis (M.S.)--Oklahoma State University, 2023.
506 $a This item must not be sold to any third party vendors.
506 $a This item must not be added to any third party search indexes.
520 $a Modern unmanned aircraft in both the research and hobby fields often rely on hobby grade sensors for detection of airspeed and differential pressures. These sensors are used by both pilots and autopilot systems for control of the airframe, however the limits of these systems and their implementations are often not adequately understood. A full wind tunnel calibration of airframes with installed sensors would greatly reduce the errors before flight, but this is often not feasible due to size of aircraft or available facilities. This leaves most error correction to be done by flight testing which requires the risking of the airframe with potentially poor calibration values. Proper analysis of expected errors from probe type and placement are necessary to mitigate the risks to airspeed dependent airframes before they are able to gather the appropriate flight data for airspeed corrections. In addition to the standard error correction, a proper uncertainty analysis should be performed for all used sensors to ensure the feasibility of the measurements they are trying to obtain. This combination of analyses can be used to provide guidance for obtaining an airspeed measurement as well as other potential air data values. Angle of attack measurement is rarely available on small UAS systems, likely due to installation issues and lack of sensor accuracy over broad speed ranges. Similar to airspeed, general guidance and feasibility studies can be performed using expected errors and uncertainty analysis to determine the potential for using common airspeed sensors for the detection of an airframe's angle of attack.
590 $a School code: 0664.
650 4 $a Aerospace engineering. $3 1002622
650 4 $a Engineering. $3 586835
650 4 $a Fluid mechanics. $3 528155
653 $a Aircraft
653 $a Autopilot systems
653 $a Airframes
653 $a Calibration values
690 $a 0538
690 $a 0537
690 $a 0204
710 2 $a Oklahoma State University. $b Mechanical & Aerospace Engineering. $3 3194223
773 0 $t Masters Abstracts International $g 85-07.
790 $a 0664
791 $a M.S.
792 $a 2023
793 $a English
856 4 0 $u https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=30575871