Zobrazeno 1 - 10
of 20
pro vyhledávání: '"Morteza Tayefi"'
Autor:
Moslem Karim Abadeh, Morteza Tayefi
Publikováno v:
فصلنامه علوم و فناوری فضایی, Vol 17, Iss 3, Pp 15-27 (2024)
This study explores the control of a space capsule during the re-entry phase. Spacecraft re-entry is a critical phase of a mission because, as the spacecraft enters Earth's atmosphere, aerodynamic forces and moments can disturb the angles of attack a
Externí odkaz:
https://doaj.org/article/6e270e4984374693a329799c8fbcf095
Autor:
Morteza Tayefi, Ramin Kamali Moghadam
Publikováno v:
فصلنامه علوم و فناوری فضایی, Vol 15, Iss 3, Pp 1-9 (2022)
To create drag and reduce the speed of space payloads in the phase of entering the atmosphere, the payload body itself can be used as brake mechanisms without using additional tools. The approach analyzed in this paper is the separation of the nose a
Externí odkaz:
https://doaj.org/article/1958c4dc15774b88b7d3c5d52f61c886
Publikováno v:
فصلنامه علوم و فناوری فضایی, Vol 12, Iss 4, Pp 69-77 (2019)
Sounding rockets provide a useful platform for the aerospace research activities in which carry out a research payload to the space and recover it in the ground. In the flight path, it does scientific experiments and acquire the result for more analy
Externí odkaz:
https://doaj.org/article/de2a3cbc9bf941a18b13c112ea3bcb36
Publikováno v:
International Journal of Intelligent Unmanned Systems.
PurposeThis study aims to minimize the risk of costly failures of flight tests during the path tracking control design, and a noble approach has been proposed in this study to put the whole vehicle-in-the simulation loop. Working with the real system
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6d574bda9783ea8681f684a0a1475d87
https://doi.org/10.1108/ijius-06-2022-0085
https://doi.org/10.1108/ijius-06-2022-0085
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. :095441002211488
This paper addresses the attitude path design of a remote sensing satellite in various imaging modes. The novel path design algorithm is based on local polynomial regression, which produces a smooth attitude path by receiving the size and timing of m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c073fe44c8b8a9527e1756225ed7e815
https://doi.org/10.1177/09544100221148887
https://doi.org/10.1177/09544100221148887
Autor:
Zhiyong Geng, Morteza Tayefi
Publikováno v:
Journal of Intelligent & Robotic Systems. 90:253-265
This work presents a novel geometric framework for self-balancing as well as planar motion control of wheeled vehicles with two fewer control inputs than the configuration variables. For self-balancing control, we shape the kinetic energy in such a w
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fa888002221e277d006c7a276cadd164
https://doi.org/10.1007/s10846-017-0666-7
https://doi.org/10.1007/s10846-017-0666-7
Logarithmic control, trajectory tracking, and formation for nonholonomic vehicles on Lie group SE(2)
Autor:
Morteza Tayefi, Zhiyong Geng
Publikováno v:
International Journal of Control. 92:204-224
This paper studies the problem of set-point stabilisation, trajectory tracking, and formation tracking for unicycle-type vehicles by taking advantage of the exponential coordinates and the other mathematical tools provided by the Lie group setting of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::413944936737c4c1220e342cfb1653ee
https://doi.org/10.1080/00207179.2017.1349341
https://doi.org/10.1080/00207179.2017.1349341
Publikováno v:
Nonlinear Dynamics. 87:665-675
This paper addresses the problem of consensus and formation control for nonholonomic multivehicle systems. The problem is formulated using the definition of the convex combination on SE(2) which simultaneously preserves the nonholonomic constraint in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::36e705691b01d012ace19ad7f39ac874
https://doi.org/10.1007/s11071-016-3067-8
https://doi.org/10.1007/s11071-016-3067-8
Publikováno v:
Aerospace Science and Technology. 107:106238
This paper presents a novel concept of a co-axial bi-rotor UAV which is controlled by moving its center of gravity. After deriving a 6DOF nonlinear model using the Euler-Newton method, we introduce a simplified 3DOF model for planar motion. Due to th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::306178156c2824cdd4326266c676859c
https://doi.org/10.1016/j.ast.2020.106238
https://doi.org/10.1016/j.ast.2020.106238
Autor:
Morteza Tayefi, Zhiyong Geng
Publikováno v:
2016 Chinese Control and Decision Conference (CCDC).
This work presents a controlled Lagrangian for the wheeled inverted pendulum system in which the upward position of the pendulum becomes a stable nonlinear equilibrium. Unlike the general form of underactuated systems, the configuration variables are
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0f4b40654d88b84974ce5d63b4fa9697
https://doi.org/10.1109/ccdc.2016.7531269
https://doi.org/10.1109/ccdc.2016.7531269