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Titlebook: Embedded Platforms for UAS Landing Path and Obstacle Detection; Integration and Deve Umberto Papa Book 20181st edition Springer Internation

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發(fā)表于 2025-3-21 19:52:24 | 只看該作者 |倒序?yàn)g覽 |閱讀模式
書(shū)目名稱(chēng)Embedded Platforms for UAS Landing Path and Obstacle Detection
副標(biāo)題Integration and Deve
編輯Umberto Papa
視頻videohttp://file.papertrans.cn/308/307912/307912.mp4
概述Offers useful insights into sensor design and fusion for unmanned aircraft systems.Describes a method for finding the best path and landing site, upon detection of any obstacle in the zone.Reports on
叢書(shū)名稱(chēng)Studies in Systems, Decision and Control
圖書(shū)封面Titlebook: Embedded Platforms for UAS Landing Path and Obstacle Detection; Integration and Deve Umberto Papa Book 20181st edition Springer Internation
描述This book reports on the design and development of a system that assists remote pilots during the landing procedure. In particular, it covers a previously neglected topic, namely the search for the best pathway and landing site. It describes the system’s components, such as the ultrasonic sensor, infrared sensor and optical sensor, in detail, and discusses the experimental tests carried out in both controlled laboratory and real-world environments. Providing a fascinating survey of the state of the art in the field of unmanned aircraft system electronics design and development, the book also presents recent advances in and cutting-edge methodologies for the development of acquisition systems and inexpensive sensor design for navigation data.
出版日期Book 20181st edition
關(guān)鍵詞UAS Safe Landing; Flight Mechanics; Sensors Fusion; Aircraft Design; Obstacle Detection and Avoidance; Ul
版次1
doihttps://doi.org/10.1007/978-3-319-73174-2
isbn_softcover978-3-319-89237-5
isbn_ebook978-3-319-73174-2Series ISSN 2198-4182 Series E-ISSN 2198-4190
issn_series 2198-4182
copyrightSpringer International Publishing AG 2018
The information of publication is updating

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沙發(fā)
發(fā)表于 2025-3-21 23:35:13 | 只看該作者
edded sensors platform useful to assist the remote pilot during the landing procedure. The design and implementation of an electronic platform were performed by using a bouquet of low-cost sensors (ultrasonic, IR, Optics, etc.) for attitude control and obstacle-sense-and-avoid during the landing procedure at low altitude and low velocity.
板凳
發(fā)表于 2025-3-22 02:14:33 | 只看該作者
Reduction of the Number of Variables,ant limitations on the total size, weight, and power requirements of potential sensors. In this chapter, a Sonic Ranging (SR) sensor was used in order to detect any oblacles that surround the UAV. The system proposed it is able to detect obstacles like dolphins or bats do.
地板
發(fā)表于 2025-3-22 05:29:04 | 只看該作者
5#
發(fā)表于 2025-3-22 12:06:03 | 只看該作者
Book 20181st editionusly neglected topic, namely the search for the best pathway and landing site. It describes the system’s components, such as the ultrasonic sensor, infrared sensor and optical sensor, in detail, and discusses the experimental tests carried out in both controlled laboratory and real-world environment
6#
發(fā)表于 2025-3-22 14:21:45 | 只看該作者
Introduction to Unmanned Aircraft Systems (UAS),edded sensors platform useful to assist the remote pilot during the landing procedure. The design and implementation of an electronic platform were performed by using a bouquet of low-cost sensors (ultrasonic, IR, Optics, etc.) for attitude control and obstacle-sense-and-avoid during the landing procedure at low altitude and low velocity.
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發(fā)表于 2025-3-22 18:15:37 | 只看該作者
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發(fā)表于 2025-3-22 22:35:14 | 只看該作者
Atmosphere Effects on the SRS,rricane Ike in Galveston, Texas, US). Unfortunately, the measurements provided by ultrasonic sensors are affected by systematic errors due to relative humidity and atmospheric conditions. This chapter explains a method useful to correct, in real time, errors given by temperature and relative humidity on the sonar sensors measurements.
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發(fā)表于 2025-3-23 03:19:05 | 只看該作者
10#
發(fā)表于 2025-3-23 06:51:43 | 只看該作者
UAS Endurance Enhancement,r focuses on the flight time of the vehicle and proposes an alternative approach to improve the endurance of a non-expensive, commercial quadrotor, by applying a balloon to reduce weight and power consumption needed for flight.
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