ORCID Profile
0000-0002-8016-0914
Current Organisation
University of Sydney
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Photogrammetry and Remote Sensing | Aerospace Engineering | Astronomical and Space Instrumentation | Satellite, Space Vehicle and Missile Design and Testing
Aerospace Equipment | Expanding Knowledge in the Environmental Sciences | Scientific Instruments |
Publisher: Elsevier BV
Date: 11-2016
Publisher: IEEE
Date: 08-2011
Publisher: AIP Publishing
Date: 2018
DOI: 10.1063/1.5004004
Abstract: This paper develops a drone control prototype based on web technology with the aid of hand gesture. The uplink control command and downlink data (e.g., video) are transmitted by WiFi communication, and all the information exchange is realized on web. The control command is translated from various predetermined hand gestures. Specifically, the hardware of this friendly interactive control system is composed by a quadrotor drone, a computer vision-based hand gesture sensor, and a cost-effective computer. The software is simplified as a web-based user interface program. Aided by natural hand gestures, this system significantly reduces the complexity of traditional human-computer interaction, making remote drone operation more intuitive. Meanwhile, a web-based automatic control mode is provided in addition to the hand gesture control mode. For both operation modes, no extra application program is needed to be installed on the computer. Experimental results demonstrate the effectiveness and efficiency of the proposed system, including control accuracy, operation latency, etc. This system can be used in many applications such as controlling a drone in global positioning system denied environment or by handlers without professional drone control knowledge since it is easy to get started.
Publisher: Science Publications
Date: 2010
Publisher: IEEE
Date: 12-2009
Publisher: Elsevier BV
Date: 10-2017
Publisher: Elsevier BV
Date: 09-2018
Publisher: Elsevier BV
Date: 03-2017
Publisher: IEEE
Date: 08-2007
DOI: 10.1109/AHS.2007.39
Publisher: IEEE
Date: 07-2014
Publisher: IEEE
Date: 10-2014
Publisher: IEEE
Date: 09-2015
Publisher: IEEE
Date: 06-2010
Publisher: IEEE
Date: 06-2016
Publisher: IEEE
Date: 06-2008
DOI: 10.1109/AHS.2008.55
Publisher: Institute of Electrical and Electronics Engineers (IEEE)
Date: 2020
Publisher: IOP Publishing
Date: 06-07-2016
Publisher: Institute of Electrical and Electronics Engineers (IEEE)
Date: 03-2018
Publisher: IEEE
Date: 06-2016
Publisher: Springer Science and Business Media LLC
Date: 03-03-2016
Publisher: IEEE
Date: 08-2007
DOI: 10.1109/AHS.2007.44
Publisher: Elsevier BV
Date: 09-2018
Publisher: IEEE
Date: 2006
DOI: 10.1109/AHS.2006.33
Publisher: IEEE
Date: 06-2008
DOI: 10.1109/AHS.2008.56
Publisher: Elsevier BV
Date: 04-2021
Publisher: Elsevier BV
Date: 11-2016
Publisher: IEEE
Date: 07-2012
Publisher: IEEE
Date: 07-2012
Publisher: Elsevier BV
Date: 05-2018
Publisher: IEEE
Date: 03-2008
Publisher: Elsevier BV
Date: 09-2023
Publisher: IEEE
Date: 06-2015
Publisher: Informa UK Limited
Date: 10-2022
DOI: 10.1080/14763141.2019.1649715
Abstract: This investigation sought to quantify the level of measurement agreement in system force, velocity and power values derived across three commonly applied assessment techniques during a countermovement jump (CMJ). Twenty-five male national representative athletes completed three CMJs under unloaded (0%
Publisher: Institute of Electrical and Electronics Engineers (IEEE)
Date: 02-2023
Publisher: SPIE
Date: 22-08-2012
DOI: 10.1117/12.925709
Publisher: IEEE
Date: 06-2011
Publisher: Institute of Electrical and Electronics Engineers (IEEE)
Date: 2023
Publisher: Elsevier BV
Date: 05-2017
Publisher: Institute of Electrical and Electronics Engineers (IEEE)
Date: 03-2008
Publisher: Institute of Electrical and Electronics Engineers (IEEE)
Date: 2023
Publisher: Elsevier BV
Date: 07-2018
Publisher: Institute of Electrical and Electronics Engineers (IEEE)
Date: 04-2017
Publisher: Hindawi Limited
Date: 12-11-2020
DOI: 10.1155/2020/7503272
Abstract: According to the trajectory specialty of hypersonic boost-glide vehicles, a strapdown inertial navigation system/BeiDou navigation satellite system (SINS/BDS) algorithm based on the launch-centered inertial (LCI) frame for hypersonic vehicles is proposed. First, the related frame system, especially the launch earth-centered inertial (LECI) frame, and the SINS mechanization in the LCI frame are introduced. Second, SINS discrete updating algorithms in the LCI frame for the compensation of coning, sculling, and scrolling effects are deduced in the attitude, velocity, and position updating algorithms, respectively. Subsequently, the Kalman filter of the SINS/BDS integrated navigation in the LCI frame is obtained. The method of converting BDS receiver position and velocity from the Earth-centered Earth-fixed (ECEF) frame to the LCI frame is deduced through the LECI frame. Finally, taking the typical hypersonic boost-glide vehicles as the object, the SINS/BDS algorithm vehicle field test and hardware-in-the-loop simulation are performed.
Publisher: Elsevier BV
Date: 02-2014
Publisher: Elsevier BV
Date: 07-2018
Publisher: IEEE
Date: 03-2008
Publisher: IEEE
Date: 12-2010
Publisher: Elsevier BV
Date: 04-2017
Publisher: IEEE
Date: 2006
DOI: 10.1109/AHS.2006.54
Publisher: IEEE
Date: 08-2013
Publisher: Elsevier BV
Date: 03-2016
Publisher: Elsevier BV
Date: 10-2017
Publisher: IEEE
Date: 06-2011
Location: United Kingdom of Great Britain and Northern Ireland
Location: United Kingdom of Great Britain and Northern Ireland
Start Date: 12-2017
End Date: 12-2024
Amount: $4,619,950.00
Funder: Australian Research Council
View Funded Activity