Effects of Variable Arm Length on UAV Control Systems

Abstract Quadrotor is a type of unmanned aerial vehicle that has been widely used in many applications, such as, policing, surveillance, aerial photography and agriculture. Conventionally, the control of quadrotor flight direction is accomplished by varying speeds of rotors or manipulating torques....
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Autor*in:	Rizon, M. [verfasserIn] Ang, C. K. Solihin, Mahmud Iwan Razlan, Zuradzman Mohamad Desa, Hazy Bakar, Shahriman A. Khairunizam, Wan Ibrahim, Zunaidi

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2020

Schlagwörter:	UAV quadrotor moment of bending arm length

Anmerkung:	© The Authors 2020

Übergeordnetes Werk:	Enthalten in: Journal of Robotics, Networking and Artificial Life - Springer Netherlands, 2014, 7(2020), 2 vom: 03. Juni, Seite 91-97
Übergeordnetes Werk:	volume:7 ; year:2020 ; number:2 ; day:03 ; month:06 ; pages:91-97

Links:	Volltext

DOI / URN:	10.2991/jrnal.k.200528.004

Katalog-ID:	SPR055095992

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520			\|a Abstract Quadrotor is a type of unmanned aerial vehicle that has been widely used in many applications, such as, policing, surveillance, aerial photography and agriculture. Conventionally, the control of quadrotor flight direction is accomplished by varying speeds of rotors or manipulating torques. In this paper, a novel mechanism is proposed. The mechanism uses stepper rotors to control the arm length for changing flight directions, while maintaining rotors’ speed at constant. This can be achieved using a mathematical analysis of relation between quadrotor arm length and moment of bending of various position of rotor. Analysis and simulation results have shown the change in arm length required to produce moment of bending for hovering, roll and pitch motion. Experimental results have shown that the new mechanism is able to carry more payloads which the rotor speed can be utilized fully at 100% while the flight direction is been controlled by changing of the arm length compared to conventional flight control mechanisms.
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allfields	10.2991/jrnal.k.200528.004 doi (DE-627)SPR055095992 (SPR)jrnal.k.200528.004-e DE-627 ger DE-627 rakwb eng Rizon, M. verfasserin aut Effects of Variable Arm Length on UAV Control Systems 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Authors 2020 Abstract Quadrotor is a type of unmanned aerial vehicle that has been widely used in many applications, such as, policing, surveillance, aerial photography and agriculture. Conventionally, the control of quadrotor flight direction is accomplished by varying speeds of rotors or manipulating torques. In this paper, a novel mechanism is proposed. The mechanism uses stepper rotors to control the arm length for changing flight directions, while maintaining rotors’ speed at constant. This can be achieved using a mathematical analysis of relation between quadrotor arm length and moment of bending of various position of rotor. Analysis and simulation results have shown the change in arm length required to produce moment of bending for hovering, roll and pitch motion. Experimental results have shown that the new mechanism is able to carry more payloads which the rotor speed can be utilized fully at 100% while the flight direction is been controlled by changing of the arm length compared to conventional flight control mechanisms. UAV (dpeaa)DE-He213 quadrotor (dpeaa)DE-He213 moment of bending (dpeaa)DE-He213 arm length (dpeaa)DE-He213 Ang, C. K. aut Solihin, Mahmud Iwan aut Razlan, Zuradzman Mohamad aut Desa, Hazy aut Bakar, Shahriman A. aut Khairunizam, Wan aut Ibrahim, Zunaidi aut Enthalten in Journal of Robotics, Networking and Artificial Life Springer Netherlands, 2014 7(2020), 2 vom: 03. Juni, Seite 91-97 (DE-627)1005552487 (DE-600)2912430-X 2352-6386 nnns volume:7 year:2020 number:2 day:03 month:06 pages:91-97 https://dx.doi.org/10.2991/jrnal.k.200528.004 kostenfrei Volltext SYSFLAG_0 GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 7 2020 2 03 06 91-97
spelling	10.2991/jrnal.k.200528.004 doi (DE-627)SPR055095992 (SPR)jrnal.k.200528.004-e DE-627 ger DE-627 rakwb eng Rizon, M. verfasserin aut Effects of Variable Arm Length on UAV Control Systems 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Authors 2020 Abstract Quadrotor is a type of unmanned aerial vehicle that has been widely used in many applications, such as, policing, surveillance, aerial photography and agriculture. Conventionally, the control of quadrotor flight direction is accomplished by varying speeds of rotors or manipulating torques. In this paper, a novel mechanism is proposed. The mechanism uses stepper rotors to control the arm length for changing flight directions, while maintaining rotors’ speed at constant. This can be achieved using a mathematical analysis of relation between quadrotor arm length and moment of bending of various position of rotor. Analysis and simulation results have shown the change in arm length required to produce moment of bending for hovering, roll and pitch motion. Experimental results have shown that the new mechanism is able to carry more payloads which the rotor speed can be utilized fully at 100% while the flight direction is been controlled by changing of the arm length compared to conventional flight control mechanisms. UAV (dpeaa)DE-He213 quadrotor (dpeaa)DE-He213 moment of bending (dpeaa)DE-He213 arm length (dpeaa)DE-He213 Ang, C. K. aut Solihin, Mahmud Iwan aut Razlan, Zuradzman Mohamad aut Desa, Hazy aut Bakar, Shahriman A. aut Khairunizam, Wan aut Ibrahim, Zunaidi aut Enthalten in Journal of Robotics, Networking and Artificial Life Springer Netherlands, 2014 7(2020), 2 vom: 03. Juni, Seite 91-97 (DE-627)1005552487 (DE-600)2912430-X 2352-6386 nnns volume:7 year:2020 number:2 day:03 month:06 pages:91-97 https://dx.doi.org/10.2991/jrnal.k.200528.004 kostenfrei Volltext SYSFLAG_0 GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 7 2020 2 03 06 91-97
allfields_unstemmed	10.2991/jrnal.k.200528.004 doi (DE-627)SPR055095992 (SPR)jrnal.k.200528.004-e DE-627 ger DE-627 rakwb eng Rizon, M. verfasserin aut Effects of Variable Arm Length on UAV Control Systems 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Authors 2020 Abstract Quadrotor is a type of unmanned aerial vehicle that has been widely used in many applications, such as, policing, surveillance, aerial photography and agriculture. Conventionally, the control of quadrotor flight direction is accomplished by varying speeds of rotors or manipulating torques. In this paper, a novel mechanism is proposed. The mechanism uses stepper rotors to control the arm length for changing flight directions, while maintaining rotors’ speed at constant. This can be achieved using a mathematical analysis of relation between quadrotor arm length and moment of bending of various position of rotor. Analysis and simulation results have shown the change in arm length required to produce moment of bending for hovering, roll and pitch motion. Experimental results have shown that the new mechanism is able to carry more payloads which the rotor speed can be utilized fully at 100% while the flight direction is been controlled by changing of the arm length compared to conventional flight control mechanisms. UAV (dpeaa)DE-He213 quadrotor (dpeaa)DE-He213 moment of bending (dpeaa)DE-He213 arm length (dpeaa)DE-He213 Ang, C. K. aut Solihin, Mahmud Iwan aut Razlan, Zuradzman Mohamad aut Desa, Hazy aut Bakar, Shahriman A. aut Khairunizam, Wan aut Ibrahim, Zunaidi aut Enthalten in Journal of Robotics, Networking and Artificial Life Springer Netherlands, 2014 7(2020), 2 vom: 03. Juni, Seite 91-97 (DE-627)1005552487 (DE-600)2912430-X 2352-6386 nnns volume:7 year:2020 number:2 day:03 month:06 pages:91-97 https://dx.doi.org/10.2991/jrnal.k.200528.004 kostenfrei Volltext SYSFLAG_0 GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 7 2020 2 03 06 91-97
allfieldsGer	10.2991/jrnal.k.200528.004 doi (DE-627)SPR055095992 (SPR)jrnal.k.200528.004-e DE-627 ger DE-627 rakwb eng Rizon, M. verfasserin aut Effects of Variable Arm Length on UAV Control Systems 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Authors 2020 Abstract Quadrotor is a type of unmanned aerial vehicle that has been widely used in many applications, such as, policing, surveillance, aerial photography and agriculture. Conventionally, the control of quadrotor flight direction is accomplished by varying speeds of rotors or manipulating torques. In this paper, a novel mechanism is proposed. The mechanism uses stepper rotors to control the arm length for changing flight directions, while maintaining rotors’ speed at constant. This can be achieved using a mathematical analysis of relation between quadrotor arm length and moment of bending of various position of rotor. Analysis and simulation results have shown the change in arm length required to produce moment of bending for hovering, roll and pitch motion. Experimental results have shown that the new mechanism is able to carry more payloads which the rotor speed can be utilized fully at 100% while the flight direction is been controlled by changing of the arm length compared to conventional flight control mechanisms. UAV (dpeaa)DE-He213 quadrotor (dpeaa)DE-He213 moment of bending (dpeaa)DE-He213 arm length (dpeaa)DE-He213 Ang, C. K. aut Solihin, Mahmud Iwan aut Razlan, Zuradzman Mohamad aut Desa, Hazy aut Bakar, Shahriman A. aut Khairunizam, Wan aut Ibrahim, Zunaidi aut Enthalten in Journal of Robotics, Networking and Artificial Life Springer Netherlands, 2014 7(2020), 2 vom: 03. Juni, Seite 91-97 (DE-627)1005552487 (DE-600)2912430-X 2352-6386 nnns volume:7 year:2020 number:2 day:03 month:06 pages:91-97 https://dx.doi.org/10.2991/jrnal.k.200528.004 kostenfrei Volltext SYSFLAG_0 GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 7 2020 2 03 06 91-97
allfieldsSound	10.2991/jrnal.k.200528.004 doi (DE-627)SPR055095992 (SPR)jrnal.k.200528.004-e DE-627 ger DE-627 rakwb eng Rizon, M. verfasserin aut Effects of Variable Arm Length on UAV Control Systems 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Authors 2020 Abstract Quadrotor is a type of unmanned aerial vehicle that has been widely used in many applications, such as, policing, surveillance, aerial photography and agriculture. Conventionally, the control of quadrotor flight direction is accomplished by varying speeds of rotors or manipulating torques. In this paper, a novel mechanism is proposed. The mechanism uses stepper rotors to control the arm length for changing flight directions, while maintaining rotors’ speed at constant. This can be achieved using a mathematical analysis of relation between quadrotor arm length and moment of bending of various position of rotor. Analysis and simulation results have shown the change in arm length required to produce moment of bending for hovering, roll and pitch motion. Experimental results have shown that the new mechanism is able to carry more payloads which the rotor speed can be utilized fully at 100% while the flight direction is been controlled by changing of the arm length compared to conventional flight control mechanisms. UAV (dpeaa)DE-He213 quadrotor (dpeaa)DE-He213 moment of bending (dpeaa)DE-He213 arm length (dpeaa)DE-He213 Ang, C. K. aut Solihin, Mahmud Iwan aut Razlan, Zuradzman Mohamad aut Desa, Hazy aut Bakar, Shahriman A. aut Khairunizam, Wan aut Ibrahim, Zunaidi aut Enthalten in Journal of Robotics, Networking and Artificial Life Springer Netherlands, 2014 7(2020), 2 vom: 03. Juni, Seite 91-97 (DE-627)1005552487 (DE-600)2912430-X 2352-6386 nnns volume:7 year:2020 number:2 day:03 month:06 pages:91-97 https://dx.doi.org/10.2991/jrnal.k.200528.004 kostenfrei Volltext SYSFLAG_0 GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 7 2020 2 03 06 91-97
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authorswithroles_txt_mv	Rizon, M. @@aut@@ Ang, C. K. @@aut@@ Solihin, Mahmud Iwan @@aut@@ Razlan, Zuradzman Mohamad @@aut@@ Desa, Hazy @@aut@@ Bakar, Shahriman A. @@aut@@ Khairunizam, Wan @@aut@@ Ibrahim, Zunaidi @@aut@@
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author	Rizon, M.
spellingShingle	Rizon, M. misc UAV misc quadrotor misc moment of bending misc arm length Effects of Variable Arm Length on UAV Control Systems
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topic_title	Effects of Variable Arm Length on UAV Control Systems UAV (dpeaa)DE-He213 quadrotor (dpeaa)DE-He213 moment of bending (dpeaa)DE-He213 arm length (dpeaa)DE-He213
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title	Effects of Variable Arm Length on UAV Control Systems
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title_sort	effects of variable arm length on uav control systems
title_auth	Effects of Variable Arm Length on UAV Control Systems
abstract	Abstract Quadrotor is a type of unmanned aerial vehicle that has been widely used in many applications, such as, policing, surveillance, aerial photography and agriculture. Conventionally, the control of quadrotor flight direction is accomplished by varying speeds of rotors or manipulating torques. In this paper, a novel mechanism is proposed. The mechanism uses stepper rotors to control the arm length for changing flight directions, while maintaining rotors’ speed at constant. This can be achieved using a mathematical analysis of relation between quadrotor arm length and moment of bending of various position of rotor. Analysis and simulation results have shown the change in arm length required to produce moment of bending for hovering, roll and pitch motion. Experimental results have shown that the new mechanism is able to carry more payloads which the rotor speed can be utilized fully at 100% while the flight direction is been controlled by changing of the arm length compared to conventional flight control mechanisms. © The Authors 2020
abstractGer	Abstract Quadrotor is a type of unmanned aerial vehicle that has been widely used in many applications, such as, policing, surveillance, aerial photography and agriculture. Conventionally, the control of quadrotor flight direction is accomplished by varying speeds of rotors or manipulating torques. In this paper, a novel mechanism is proposed. The mechanism uses stepper rotors to control the arm length for changing flight directions, while maintaining rotors’ speed at constant. This can be achieved using a mathematical analysis of relation between quadrotor arm length and moment of bending of various position of rotor. Analysis and simulation results have shown the change in arm length required to produce moment of bending for hovering, roll and pitch motion. Experimental results have shown that the new mechanism is able to carry more payloads which the rotor speed can be utilized fully at 100% while the flight direction is been controlled by changing of the arm length compared to conventional flight control mechanisms. © The Authors 2020
abstract_unstemmed	Abstract Quadrotor is a type of unmanned aerial vehicle that has been widely used in many applications, such as, policing, surveillance, aerial photography and agriculture. Conventionally, the control of quadrotor flight direction is accomplished by varying speeds of rotors or manipulating torques. In this paper, a novel mechanism is proposed. The mechanism uses stepper rotors to control the arm length for changing flight directions, while maintaining rotors’ speed at constant. This can be achieved using a mathematical analysis of relation between quadrotor arm length and moment of bending of various position of rotor. Analysis and simulation results have shown the change in arm length required to produce moment of bending for hovering, roll and pitch motion. Experimental results have shown that the new mechanism is able to carry more payloads which the rotor speed can be utilized fully at 100% while the flight direction is been controlled by changing of the arm length compared to conventional flight control mechanisms. © The Authors 2020
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title_short	Effects of Variable Arm Length on UAV Control Systems
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