المؤلفون: Yu Wang, Jiyan Yu, Xiaoming Wang, Jia Fangxiu

المصدر: Defence Technology, Vol 33, Iss , Pp 494-505 (2024)

مصطلحات موضوعية: Spin-stabilized projectile, Reduced information, Path-following control, Extended state observer, Coupled nonlinear system, Input saturation, Military Science

وصف الملف: electronic resource

Relation: http://www.sciencedirect.com/science/article/pii/S2214914723001915; https://doaj.org/toc/2214-9147

URL الوصول: https://doaj.org/article/d6ea5fc15140468188e1be5cc874c074

المؤلفون: Косовцов, Юрій Миколайович, Грабчак, Володимир Іванович

المصدر: Озброєння та військова техніка; Том 29 № 1 (2021); 28-35 ; Вооружение и военная техника; Том 29 № 1 (2021); 28-35 ; Weapons and military equipment; Vol. 29 No. 1 (2021); 28-35 ; 2663-5550 ; 2414-0651 ; 10.34169/2414-0651.2021.1(29)

مصطلحات موضوعية: відновлення аеродинамічних коефіцієнтів, снаряд, що стабілізується обертанням, експериментальні дані вільного руху снаряда, обернена задача, модифікована модель точкової маси, identification of aerodynamic coefficients, spin stabilized projectile, free flight data, nonlinear model, inverse problem, the modified pointmass trajectory model

وصف الملف: application/pdf

Relation: https://journal.cndiovt.com.ua/index.php/ovt/article/view/577/379; https://journal.cndiovt.com.ua/index.php/ovt/article/view/577

الاتاحة: https://journal.cndiovt.com.ua/index.php/ovt/article/view/577
https://doi.org/10.34169/2414-0651.2021.1(29).28-35

المؤلفون: Jisi Cheng, Qiang Shen, Zhaowei Deng, Zilong Deng

المصدر: Electronics; Volume 8; Issue 10; Pages: 1135

مصطلحات موضوعية: spin-stabilized projectile, fixed canards, course correction fuze, dynamic control, correction features

وصف الملف: application/pdf

Relation: Systems & Control Engineering; https://dx.doi.org/10.3390/electronics8101135

الاتاحة: https://doi.org/10.3390/electronics8101135

المؤلفون: Tallec, Thomas

المساهمون: Normandie, Delvare, Franck

مصطلحات موضوعية: Coefficients aérodynamiques, Méthode inverse, Projectile gyrostabilisé, Radar de trajectographie, Aerodynamic coefficients, Asymptotic development, Inverse method, Spin stabilized projectile, Tracking radar

Relation: http://www.theses.fr/2023NORMC246/document

الاتاحة: http://www.theses.fr/2023NORMC246/document

المؤلفون: Tallec, Thomas

المساهمون: Laboratoire de Mathématiques Nicolas Oresme (LMNO), Université de Caen Normandie (UNICAEN), Normandie Université (NU)-Normandie Université (NU)-Centre National de la Recherche Scientifique (CNRS), Normandie Université, Franck Delvare

المصدر: https://theses.hal.science/tel-04426316 ; Mécanique [physics.med-ph]. Normandie Université, 2023. Français. ⟨NNT : 2023NORMC246⟩.

مصطلحات موضوعية: Aerodynamic coefficients, Asymptotic development, Inverse method, Spin stabilized projectile, Tracking radar, Coefficients aérodynamiques, Méthode inverse, Projectile gyrostabilisé, Radar de trajectographie, [SPI.MECA]Engineering Sciences [physics]/Mechanics [physics.med-ph]

Relation: NNT: 2023NORMC246; tel-04426316; https://theses.hal.science/tel-04426316; https://theses.hal.science/tel-04426316/document; https://theses.hal.science/tel-04426316/file/sygal_fusion_39127-tallec-thomas_65b8ebd222d59.pdf

الاتاحة: https://theses.hal.science/tel-04426316
https://theses.hal.science/tel-04426316/document
https://theses.hal.science/tel-04426316/file/sygal_fusion_39127-tallec-thomas_65b8ebd222d59.pdf

المؤلفون: Arnoult, Guillaume

المساهمون: DAAA, ONERA, Université Paris-Saclay [Châtillon], ONERA-Université Paris-Saclay, Université Paris-Saclay, Eric Garnier

المصدر: Mécanique des fluides [physics.class-ph]. Université Paris-Saclay, 2020. Français. ⟨NNT : 2020UPAST068⟩

مصطلحات موضوعية: Aerodynamics, Flight Mechanics, Neural nextworks, Optimisation basée sur des méta-modèles, Kriging and cokriging, Surrogate-Based optimization, Réseaux de neurones, Mécanique du vol, Kriging et cokriging, Projectile gyrostabilisé, Spin-Stabilized Projectile, Aérodynamique, [SPI.MECA.MEFL]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Fluids mechanics [physics.class-ph]

URL الوصول: https://explore.openaire.eu/search/publication?articleId=od_______212::ffcef3c9aef7b23182b80cbdaee8415a
https://tel.archives-ouvertes.fr/tel-03151163

المؤلفون: Arnoult, Guillaume

المساهمون: DAAA, ONERA, Université Paris-Saclay [Châtillon], ONERA-Université Paris-Saclay, Université Paris-Saclay, Eric Garnier

المصدر: Mécanique des fluides [physics.class-ph]. Université Paris-Saclay, 2020. Français. ⟨NNT : 2020UPAST068⟩

مصطلحات موضوعية: Aerodynamics, Flight Mechanics, Neural nextworks, Optimisation basée sur des méta-modèles, Kriging and cokriging, Surrogate-Based optimization, Réseaux de neurones, Mécanique du vol, Kriging et cokriging, Projectile gyrostabilisé, Spin-Stabilized Projectile, Aérodynamique, [SPI.MECA.MEFL]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Fluids mechanics [physics.class-ph]

URL الوصول: https://explore.openaire.eu/search/publication?articleId=od______2592::ffcef3c9aef7b23182b80cbdaee8415a
https://tel.archives-ouvertes.fr/tel-03151163

المؤلفون: Arnoult, Guillaume

المساهمون: DAAA, ONERA, Université Paris-Saclay Châtillon, ONERA-Université Paris-Saclay, Université Paris-Saclay, Eric Garnier

المصدر: https://theses.hal.science/tel-03151163 ; Mécanique des fluides [physics.class-ph]. Université Paris-Saclay, 2020. Français. ⟨NNT : 2020UPAST068⟩.

مصطلحات موضوعية: Spin-Stabilized Projectile, Flight Mechanics, Surrogate-Based optimization, Aerodynamics, Kriging and cokriging, Neural nextworks, Projectile gyrostabilisé, Mécanique du vol, Optimisation basée sur des méta-modèles, Aérodynamique, Kriging et cokriging, Réseaux de neurones, [SPI.MECA.MEFL]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Fluids mechanics [physics.class-ph]

Relation: NNT: 2020UPAST068

الاتاحة: https://theses.hal.science/tel-03151163
https://theses.hal.science/tel-03151163v1/document
https://theses.hal.science/tel-03151163v1/file/85360_ARNOULT_2020_archivage.pdf

المؤلفون: Arnoult, Guillaume

المساهمون: université Paris-Saclay, Garnier, Eric

مصطلحات موضوعية: Projectile gyrostabilisé, Mécanique du vol, Optimisation basée sur des méta-modèles, Aérodynamique, Kriging et cokriging, Réseaux de neurones, Spin-Stabilized Projectile, Flight Mechanics, Surrogate-Based optimization, Aerodynamics, Kriging and cokriging, Neural nextworks

Relation: http://www.theses.fr/2020UPAST068/document

الاتاحة: http://www.theses.fr/2020UPAST068/document

المؤلفون: Altufayl, Abdullah Abdulrahman A.

المساهمون: Den Heijer, W.L., 10715541 - Den Heijer, Willem Le Roux (Supervisor)

مصطلحات موضوعية: stability of projectile, flight dynamics, six degree of freedom trajectory model, mass asymmetries, spin-stabilized projectile, aerodynamic asymmetries, impact dispersion, Asymmetric projectiles

وصف الملف: application/pdf

URL الوصول: https://explore.openaire.eu/search/publication?articleId=od______1399::bfdfc170019f89ae9defedbc72c55416
https://orcid.org/0000-0001-9374-433X

المؤلفون: Zeidler, M.

المساهمون: ONERA - The French Aerospace Lab [Lille], ONERA, UNIVERSITE DE LILLE 1, Alain MERLEN

المصدر: Mécanique des fluides [physics.class-ph]. UNIVERSITE DE LILLE 1, 2015. Français

مصطلحات موضوعية: MECANIQUE VOL, EFFET COANDA, SPIN-STABILIZED PROJECTILE, SIMULATION NUMERIQUE, LES, FLIGHT MECHANICS, NUMERICAL SIMULATION, COANDA EFFECT, PROJECTILE GYROSTABILISE, FLOW CONTROL, RANS/URANS, CONTROLE ECOULEMENT, [SPI.MECA.MEFL]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Fluids mechanics [physics.class-ph]

URL الوصول: https://explore.openaire.eu/search/publication?articleId=od______2592::8db89fcda2bf4ee6f6e3fd4607951503
https://hal.archives-ouvertes.fr/tel-01212795

المؤلفون: Zeidler, M., Garnier, E., Cayzac, R., Merlen, A.

المساهمون: ONERA - The French Aerospace Lab Lille, ONERA, Nexter Munitions, ONERA - The French Aerospace Lab Meudon, ONERA-Université Paris Saclay (COmUE), ONERA - The French Aerospace Lab Palaiseau

المصدر: ISSN: 0001-1452.

مصطلحات موضوعية: COANDA EFFECT, SPIN-STABILIZED PROJECTILE, FLOW CONTROL, FLUIDIC ACTUATOR, [SPI.MECA.MEFL]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Fluids mechanics [physics.class-ph]

Relation: hal-01226390; https://hal.science/hal-01226390

الاتاحة: https://hal.science/hal-01226390
https://doi.org/10.2514/1.J053085

المؤلفون: Zeidler, M.

المساهمون: André, Cécile, ONERA - The French Aerospace Lab [Lille], ONERA, UNIVERSITE DE LILLE 1, Alain MERLEN

المصدر: Mécanique des fluides [physics.class-ph]. UNIVERSITE DE LILLE 1, 2015. Français

مصطلحات موضوعية: MECANIQUE VOL, SPIN-STABILIZED PROJECTILE, [SPI.MECA.MEFL] Engineering Sciences [physics]/Mechanics [physics.med-ph]/Fluids mechanics [physics.class-ph], FLOW CONTROL, [SPI.MECA.MEFL]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Fluids mechanics [physics.class-ph], EFFET COANDA, SIMULATION NUMERIQUE, LES, FLIGHT MECHANICS, NUMERICAL SIMULATION, COANDA EFFECT, PROJECTILE GYROSTABILISE, RANS/URANS, CONTROLE ECOULEMENT

وصف الملف: application/pdf

URL الوصول: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::8db89fcda2bf4ee6f6e3fd4607951503
https://hal.archives-ouvertes.fr/tel-01212795

المؤلفون: Mickael Zeidler, Eric Garnier, Roxan Cayzac, Alain Merlen

المساهمون: ONERA - The French Aerospace Lab [Lille], ONERA, Nexter Munitions, ONERA - The French Aerospace Lab [Meudon], ONERA-Université Paris Saclay (COmUE), ONERA - The French Aerospace Lab [Palaiseau]

المصدر: AIAA Journal
AIAA Journal, American Institute of Aeronautics and Astronautics, 2015, 53 (5), p. 1146-1158. ⟨10.2514/1.J053085⟩

مصطلحات موضوعية: FLUIDIC ACTUATOR, Aerospace Engineering, 02 engineering and technology, FLOW CONTROL, 01 natural sciences, 010305 fluids & plasmas, [SPI.MECA.MEFL]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Fluids mechanics [physics.class-ph], Physics::Fluid Dynamics, symbols.namesake, 0203 mechanical engineering, 0103 physical sciences, Supersonic speed, COANDA EFFECT, Aerospace engineering, Coandă effect, Physics, 020301 aerospace & aeronautics, Jet (fluid), SPIN-STABILIZED PROJECTILE, Projectile, business.industry, Aerodynamics, Mechanics, Mach number, symbols, Reynolds-averaged Navier–Stokes equations, business, Freestream

URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a07f7ffba598cfcb7b7525b85f70ba99
https://hal.archives-ouvertes.fr/hal-01226390

المؤلفون: Zeidler, M.

المساهمون: ONERA - The French Aerospace Lab Lille, ONERA, UNIVERSITE DE LILLE 1, Alain MERLEN

المصدر: https://hal.science/tel-01212795 ; Mécanique des fluides [physics.class-ph]. UNIVERSITE DE LILLE 1, 2015. Français. ⟨NNT : ⟩.

مصطلحات موضوعية: NUMERICAL SIMULATION, SPIN-STABILIZED PROJECTILE, FLOW CONTROL, COANDA EFFECT, FLIGHT MECHANICS, RANS/URANS, LES, SIMULATION NUMERIQUE, CONTROLE ECOULEMENT, PROJECTILE GYROSTABILISE, EFFET COANDA, MECANIQUE VOL, [SPI.MECA.MEFL]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Fluids mechanics [physics.class-ph]

Relation: tel-01212795; https://hal.science/tel-01212795; https://hal.science/tel-01212795/document; https://hal.science/tel-01212795/file/DAAP15021.1441890602.pdf

الاتاحة: https://hal.science/tel-01212795
https://hal.science/tel-01212795/document
https://hal.science/tel-01212795/file/DAAP15021.1441890602.pdf

المؤلفون: Acar, Recep Serdar

Thesis Advisors: Demirekler, Mubeccel

مصطلحات موضوعية: QC Physics 1-999, Ballistic Target Tracking, Spin-Stabilized Projectile, Short-Range Ballistic Target, Kalman Filter, Particle Filter

وصف الملف: text/pdf

الاتاحة: http://etd.lib.metu.edu.tr/upload/12613604/index.pdf

المؤلفون: Fresconi, Frank, Plostins, Peter

المساهمون: ARMY RESEARCH LAB ABERDEEN PROVING GROUND MD WEAPONS AND MATERIALS RESEARCH DIRECTORATE

المصدر: DTIC

مصطلحات موضوعية: Ammunition and Explosives, Ballistics, SPIN STABILIZED AMMUNITION, AERODYNAMICS, AERODYNAMIC CONTROL SURFACES, PROJECTILES, FLIGHT CONTROL SYSTEMS, PRECISION, PRECISE MUNITIONS, FLIGHT DYNAMICS, SPIN-STABILIZED PROJECTILE, CONTROL MECHANISMS

وصف الملف: text/html

Relation: http://www.dtic.mil/docs/citations/ADA494194

الاتاحة: http://www.dtic.mil/docs/citations/ADA494194
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA494194

المؤلفون: Baranowski, L.

المصدر: Journal of Theoretical and Applied Mechanics.

مصطلحات موضوعية: spin-stabilized projectile, flight stability, exterior ballistics, equations of motion of projectile

URL الوصول: http://yadda.icm.edu.pl/baztech/element/bwmeta1.element.baztech-6d1a2439-d849-410b-80c2-e0e1477883f9

المؤلفون: Baranowski, L.

المصدر: Journal of Theoretical and Applied Mechanics.

مصطلحات موضوعية: exterior ballistics, equations of motion, spin-stabilized projectile, fire control systems, MPMTM

URL الوصول: http://yadda.icm.edu.pl/baztech/element/bwmeta1.element.baztech-a30fcc47-9973-4171-87c1-acfda4d5081d

المؤلفون: Baranowski, L.

المصدر: Journal of Theoretical and Applied Mechanics.

مصطلحات موضوعية: spin-stabilized projectile, flight stability, Magnus moment

URL الوصول: http://yadda.icm.edu.pl/baztech/element/bwmeta1.element.baztech-4d23646b-5c32-4a5c-b6be-cabfbdc371fd