Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Seonhyeok Kang"'
Publikováno v:
International Journal of Control, Automation and Systems. 16:1615-1628
In this work, a robust control is applied to the automation of a hydraulic excavator. Hydraulic excavators exhibit complex nonlinear behavior due to the inherent nonlinearity of the hydraulic servo system. Furthermore, the hydraulic excavator is subj
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c24a1d51c815256d2fefd875985cc1c9
https://doi.org/10.1007/s12555-017-0071-9
https://doi.org/10.1007/s12555-017-0071-9
Publikováno v:
IEEE Transactions on Automation Science and Engineering. 14:249-259
In some of recent advances in automation of construction equipment, much research has been conducted on the control of hydraulic excavators in both industry and academia for the benefit of safety and efficiency. However, most relevant works have empl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c1baf4dc9fb4cfd60095cda67754d4b4
https://doi.org/10.1109/tase.2016.2582213
https://doi.org/10.1109/tase.2016.2582213
Autor:
H. Jin Kim, Byung-Eul Jun, Seonhyeok Kang, Byunghun Choi, Min-Jea Tahk, Changhan Park, Jin-Ik Lee
Publikováno v:
Aerospace Science and Technology. 23:270-279
In this research, we explore the feasibility of a roll-pitch-yaw integrated autopilot for a high angle-of-attack missile. Investigation of the aerodynamic characteristics of a surface-to-air missile is presented, which reveals the strong effects of a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9c28467ff7512c066d34ab6114274c82
https://doi.org/10.1016/j.ast.2011.08.002
https://doi.org/10.1016/j.ast.2011.08.002
Publikováno v:
Journal of Mechanical Science and Technology. 26:205-212
Ionic polymer-metal composites (IPMCs) are promising candidates in various sensing and actuation applications due to their light weight, large bending, and low actuation voltage requirements. However, IPMCs are still in the early stage of development
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::78af7fc88f87a9f46b0a0f8810e0b514
https://doi.org/10.1007/s12206-011-0916-8
https://doi.org/10.1007/s12206-011-0916-8
Autor:
H. Jin Kim, Seonhyeok Kang
Publikováno v:
IFAC Proceedings Volumes. 44:3920-3925
Modern anti-ship missiles are required for enhancement of the survivability against anti-air defense systems of warships. In this paper, the linear quadratic differential game missile guidance law to control impact angle and time is proposed, which e
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::882f9dcc18b6f2d6ce0578ba2dde052d
https://doi.org/10.3182/20110828-6-it-1002.00805
https://doi.org/10.3182/20110828-6-it-1002.00805
Publikováno v:
Journal of Guidance, Control, and Dynamics. 32:1622-1628
This paper explores the feasibility of roll-pitch-yaw integrated autopilots for a high angle-of-attack missile. Investigation of the aerodynamic characteristics indicates strong cross-coupling effects between the motions in longitudinal and lateral d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4599193dfa819a4d81ac8571c56ddf48
https://doi.org/10.2514/1.39812
https://doi.org/10.2514/1.39812
Autor:
Jin-Ik Lee, Youn-hwan Kim, Byung-Eul Jun, H. Jin Kim, Dae-Yeon Won, Seonhyeok Kang, Byunghun Choi
Publikováno v:
International Journal of Aeronautical and Space Sciences. 9:66-75
In this work, we explore the feasibility of roll-pitch-yaw integrated autopilots for high angle-of-attack missiles. An investigation of the aerodynamic characteristics of a surface-to-air missile is presented, which reveals the strong effects of cros
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a49ea47d204ad53f23988aa18168bec2
https://doi.org/10.5139/ijass.2008.9.1.066
https://doi.org/10.5139/ijass.2008.9.1.066
Publikováno v:
AIAA Guidance, Navigation, and Control Conference.
In this paper, we investigate a roll-pitch-yaw integrated autopilot for a short-range air-to-air missile (SRAAM) in the presence of uncertainties in total aerodynamic forces and moments. To design an adaptive controller for command following of angle
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c1aec81cfc4ce8416d515c46b511c83d
https://doi.org/10.2514/6.2011-6251
https://doi.org/10.2514/6.2011-6251
Publikováno v:
AIAA Guidance, Navigation, and Control Conference.
Aerial pursuit-evasion games pose a great challenge in obtaining the analytic solutions for highly nonlinear dynamics of the pursuer and evader. This paper proposes a nonlinear model predictive method as a tool for obtaining the numerical solutions t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a0e0a9c1ca0f52513514b87bdccd3a8e
https://doi.org/10.2514/6.2010-7880
https://doi.org/10.2514/6.2010-7880