Zobrazeno 1 - 10
of 25
pro vyhledávání: '"Hossam Hendy"'
Publikováno v:
Advances in Mechanical Engineering, Vol 6 (2014)
Transfer matrix method for multibody systems (MS-TMM) is a rife method to multi-rigid-flexible-body systems dynamics model deduction due to that there are no needs to establish the global dynamics equations of the system. Its basic idea is transferri
Externí odkaz:
https://doaj.org/article/e1aadde303c7431daca925b8ba283651
Publikováno v:
Advances in Mechanical Engineering, Vol 5 (2013)
Any trajectory calculation method has three primary sources of errors, which are model error, parameter error, and initial state error. In this paper, based on initial projectile flight trajectory data measured using Doppler radar system; a new itera
Externí odkaz:
https://doaj.org/article/ebf1e11c064c4ce98724fa164e219f3b
Autor:
Ebrahim H. Kapeel, Ehab Safwat, Ahmed M. Kamel, Mohamed K. Khalil, Yehia Z. Elhalwagy, Hossam Hendy
Publikováno v:
Unmanned Systems. 11:327-350
The flight dynamics of small Unmanned Aerial Vehicles (UAVs) exhibits substantial nonlinear features which should not be ignored in simulation or analysis. In this work, a complete six degrees of freedom (6DOF) and high-fidelity simulation model of a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0fd36323a3f9e53a6708703808de36c3
https://doi.org/10.1142/s2301385023500152
https://doi.org/10.1142/s2301385023500152
Publikováno v:
Journal of Engineering Science and Military Technologies.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0b135d22a653ce4ff117a468ebbfe3e6
https://doi.org/10.21608/ejmtc.2022.166266.1238
https://doi.org/10.21608/ejmtc.2022.166266.1238
Publikováno v:
Journal of Engineering Science and Military Technologies.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::87073ef1101c71e6a5e89a50c717f9c8
https://doi.org/10.21608/ejmtc.2022.89815.1194
https://doi.org/10.21608/ejmtc.2022.89815.1194
Publikováno v:
International Journal of Automation and Control. 17:1
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8fd8d0792bc875a59ef2db2f2c31d440
https://doi.org/10.1504/ijaac.2023.10053904
https://doi.org/10.1504/ijaac.2023.10053904
Publikováno v:
2021 International Telecommunications Conference (ITC-Egypt).
Missile-target interception accuracy is mainly dependent on guidance algorithms implemented on the onboard computer. Nowadays advanced guidance algorithms are used to cope with the increasing target's capabilities. Augmented proportional navigation g
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ade7b40c67f3d58ba1febf81ba07842a
https://doi.org/10.1109/itc-egypt52936.2021.9513941
https://doi.org/10.1109/itc-egypt52936.2021.9513941
Autor:
Ahmed Omar Elfarouk, Hossam Hendy, Ahmed W. Ebrahim, Yehia Z. Elhalwagy, Ibrahim Ismail Arafa
Publikováno v:
2020 8th International Japan-Africa Conference on Electronics, Communications, and Computations (JAC-ECC).
The initial alignment of the Inertial Navigation Systems (INS) has significant importance in recent years. It is needed to ensure the accuracy and reliability of the system. For the initial alignment of Strap-down INS (SINS), Navigation Mathematical
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::863a0c929cbdde6be534189d00bc11a9
https://doi.org/10.1109/jac-ecc51597.2020.9355964
https://doi.org/10.1109/jac-ecc51597.2020.9355964
Publikováno v:
NILES
The design of missile autopilot is an essential issue as it always shares several challenges. The accuracy of impact is highly affected by designed controller accuracy and robustness against the target maneuver and missile nonlinearity resources. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::02417befa0d4bc7581f93f0b51655525
https://doi.org/10.1109/niles50944.2020.9257900
https://doi.org/10.1109/niles50944.2020.9257900
Publikováno v:
NILES
The Inertial Navigation Systems (INS), Global Navigation Satellite System (GNSS) integration becomes very important for high speed flying vehicles as a navigation solution. In this paper, a derivation and modeling of a system model of the integrated
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::280d1adcd308b680fb400b9c882176ea
https://doi.org/10.1109/niles50944.2020.9257982
https://doi.org/10.1109/niles50944.2020.9257982