Zobrazeno 1 - 10
of 87
pro vyhledávání: '"Matthew J. Rutherford"'
Publikováno v:
Drones, Vol 8, Iss 4, p 116 (2024)
Multirotor UAVs are used for a wide spectrum of civilian and public domain applications. Their navigation controllers include onboard sensor suites that facilitate safe, autonomous or semi-autonomous multirotor flight, operation, and functionality un
Externí odkaz:
https://doaj.org/article/8ffc6cef0a7f47f0a726774c218a2b7c
Publikováno v:
The Aeronautical Journal. 125:2087-2113
Backstepping represents a promising control law for fixed-wing Unmanned Aerial Vehicles (UAVs). Its non-linearity and its adaptation capabilities guarantee adequate control performance over the whole flight envelope, even when the aircraft model is a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::39bf79e80e35f1b196a5c9dc6fe215c6
https://doi.org/10.1017/aer.2021.53
https://doi.org/10.1017/aer.2021.53
Publikováno v:
Journal of Intelligent & Robotic Systems. 100:1469-1491
Model-Based Control (MBC) techniques have dominated flight controller designs for Unmanned Aerial Vehicles (UAVs). Despite their success, MBC-based designs rely heavily on the accuracy of the mathematical model of the real plant and they suffer from
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::043e971e853b59c3cf33d730ab0fda38
https://doi.org/10.1007/s10846-020-01227-8
https://doi.org/10.1007/s10846-020-01227-8
Publikováno v:
International Journal of Control, Automation and Systems. 18:801-816
This paper presents a survey of controller design techniques aimed at autonomous navigation and control of Unmanned Aerial Vehicles (UAVs), focusing on the challenge of aerodynamic uncertainty. Although many roadblocks exist, the most significant and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cfdf5359a105c9e1292030b8239ec04e
https://doi.org/10.1007/s12555-018-0489-8
https://doi.org/10.1007/s12555-018-0489-8
Publikováno v:
Control Theory and Technology. 18:1-18
This paper presents a system identification method to derive accurate mathematical models for an unmanned circulation control aerial vehicle (UC2AV) that account for the effects of circulation control (CC) on the vehicle dynamics. The X-plane flight
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1e3bed64a2acec0c22cf4808eac2e9fb
https://doi.org/10.1007/s11768-020-8151-4
https://doi.org/10.1007/s11768-020-8151-4
Autor:
Margareta Stefanovic, Kimon P. Valavanis, Mohammed Qasim, Mohammed N. Alghanim, Matthew J. Rutherford
Publikováno v:
MED
A Passivity-Based Adaptive Controller (PBAC) is derived and tested for the integrated Argo J5 Skid Steering Mobile Robot (SSMR) and custom-built landing platform. The twofold aim is to demonstrate landing platform dynamic self-leveling accuracy, coup
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9b4259da7be178d76959d8e4df1a4f45
https://doi.org/10.1109/med48518.2020.9182807
https://doi.org/10.1109/med48518.2020.9182807
Autor:
Mohammed N. Alghanim, Margareta Stefanovic, Mohammed Qasim, Kimon P. Valavanis, Matthew J. Rutherford
Publikováno v:
MED
This paper focuses on a comparative study of linear, nonlinear and adaptive controller performance to level within 1° of the horizon - regardless of terrain configuration, i.e., rough, asphalt, off-road - a custom-built landing platform for quadroto
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5ae92d9ad92dc608debc4124cb63fccc
https://doi.org/10.1109/med48518.2020.9182837
https://doi.org/10.1109/med48518.2020.9182837
Publikováno v:
2020 IEEE Aerospace Conference.
The aim of this research is to analyze a potential Mars Sample Return (MSR) mission through the study of an optimized design of the Mars Ascent Vehicle (MAV) propulsion system. The main goal of the MSR mission is to return to Earth samples of rocks a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ab357295f9127fc0dab61434f86f75ea
https://doi.org/10.1109/aero47225.2020.9172367
https://doi.org/10.1109/aero47225.2020.9172367
Publikováno v:
Springer Tracts in Autonomous Systems ISBN: 9783030407155
The proposed controller design framework has been validated for stability and navigational control of the \(UC^{2}AV\). For CC to be implemented on the \(UC^{2}AV\), a forward impeller centrifugal compressor is used, located in the fuselage and calle
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c87a20a4f2c9dab1a47a4f52d5caaaf0
https://doi.org/10.1007/978-3-030-40716-2_5
https://doi.org/10.1007/978-3-030-40716-2_5
Publikováno v:
Springer Tracts in Autonomous Systems ISBN: 9783030407155
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a5843129f2e2c4d9ccdf530e6b3590ca
https://doi.org/10.1007/978-3-030-40716-2_4
https://doi.org/10.1007/978-3-030-40716-2_4