Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Hesham A. Abdin"'
Autor:
Hesham A. Abdin, Hany M. Arnaoot
Publikováno v:
2022 International Telecommunications Conference (ITC-Egypt).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e65b1f0a9c58777ebba1feb9126513aa
https://doi.org/10.1109/itc-egypt55520.2022.9855711
https://doi.org/10.1109/itc-egypt55520.2022.9855711
Autor:
Hany M. Arnaoot, Hesham A. Abdin
Publikováno v:
2022 International Telecommunications Conference (ITC-Egypt).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::157ccf5b343c0165f872865c91608d53
https://doi.org/10.1109/itc-egypt55520.2022.9855737
https://doi.org/10.1109/itc-egypt55520.2022.9855737
Publikováno v:
2021 International Telecommunications Conference (ITC-Egypt).
The guidance of homing missiles with low-cost seekers is a common problem due to the delayed line-of-sight rate. This paper presents a novel approach to overcome this problem. The fixed navigation gain in guidance law is exchanged with a variable gai
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7b9647bdf7a2f84942ba7b51f72ade4a
https://doi.org/10.1109/itc-egypt52936.2021.9513945
https://doi.org/10.1109/itc-egypt52936.2021.9513945
Publikováno v:
2021 International Telecommunications Conference (ITC-Egypt).
The main objective of the current work is to increase onboard sensor efficiency through the selection/optimization of the ship steering control system or the adjustment of sensor parameters. Three control approaches are considered, The Linear quadrat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c3af50c34d25317ba75c7d8b0f2e3a82
https://doi.org/10.1109/itc-egypt52936.2021.9513929
https://doi.org/10.1109/itc-egypt52936.2021.9513929
Publikováno v:
2021 International Telecommunications Conference (ITC-Egypt).
In this paper, a new hybrid guidance law was presented based on the phased mixing of the proportional navigation (PN) and differential geometry (DG) guidance laws during the missile's flight stages to be able to deal with maneuvering targets, especia
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::15e5e85f060d1b7aae6848dd212ff4da
https://doi.org/10.1109/itc-egypt52936.2021.9513926
https://doi.org/10.1109/itc-egypt52936.2021.9513926