Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Elsayed M. Khalil"'
Publikováno v:
Alexandria Engineering Journal, Vol 61, Iss 12, Pp 12247-12257 (2022)
System design is a complicated and iterative process. Accordingly, a robust optimization procedure should be involved during the design process to minimize complications and time consumed for the whole process. The present research proposes a new met
Externí odkaz:
https://doaj.org/article/2e022666d4e44874aa7f25e8c3c28cc2
Publikováno v:
International Journal of Aerospace Engineering, Vol 2014 (2014)
A Steepest-Ascent numerical procedure for offline trajectory optimization of a surface-to-surface missile attacking a stationary target is presented. A detailed numerical solution, starting from building the mathematical formulation till generating a
Externí odkaz:
https://doaj.org/article/f5fae7e9ea88403db85a7473be6a313e
Publikováno v:
2022 4th Novel Intelligent and Leading Emerging Sciences Conference (NILES).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ecbb4a0e7ad3525bfd0a5341aa57c659
https://doi.org/10.1109/niles56402.2022.9942437
https://doi.org/10.1109/niles56402.2022.9942437
Publikováno v:
AIAA AVIATION 2022 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c9a45c0937dc5fb1cc09a8fad6e44a70
https://doi.org/10.2514/6.2022-3868
https://doi.org/10.2514/6.2022-3868
Publikováno v:
2021 IEEE 7th International Conference on Control Science and Systems Engineering (ICCSSE).
This study aims to provide a robust and rapid design tool to be used in the sizing of the aerodynamic surfaces of an air vehicle. This tool aims to find a globally optimum aerodynamic configuration during the considered conceptual design phase. The c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6280f6aad4479229636b923a569538a1
https://doi.org/10.1109/iccsse52761.2021.9545200
https://doi.org/10.1109/iccsse52761.2021.9545200
Publikováno v:
International Journal of Aeronautical and Space Sciences. 19:183-195
The paper proposes waypoints following guidance law. In this method an optimal trajectory is first generated which is then represented through a set of waypoints that are distributed from the starting point up to the final target point using a polyno
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b46520b4c1e401b7ad13c2c42e268036
https://doi.org/10.1007/s42405-018-0007-5
https://doi.org/10.1007/s42405-018-0007-5
Publikováno v:
International Journal of Aerospace Engineering, Vol 2019 (2019)
A numerical study has been performed to characterize the nozzle flow field of secondary injection thrust vector control (SITVC) and to estimate the performance parameters of SITVC. After validating the CFD turbulence models with an experimental data,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4a52b5c7adb553b72e766b0acf3a83e2
https://doaj.org/article/8587ad7df02e44d5bdad085a6cd3e74d
https://doaj.org/article/8587ad7df02e44d5bdad085a6cd3e74d
Publikováno v:
International Journal of Aerospace Engineering, Vol 2014 (2014)
A Steepest-Ascent numerical procedure for offline trajectory optimization of a surface-to-surface missile attacking a stationary target is presented. A detailed numerical solution, starting from building the mathematical formulation till generating a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0801817bd3204c005d7c4819a533435e
https://doaj.org/article/f5fae7e9ea88403db85a7473be6a313e
https://doaj.org/article/f5fae7e9ea88403db85a7473be6a313e