Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Dongsoo Cho"'
Autor:
Seung-Hwan Kim, Dongsoo Cho
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 234:2139-2152
A guidance problem for impact angle control applicable to a missile equipped with a passive seeker is investigated. The proposed guidance law based on the sliding mode control consists of the proportional navigation guidance term with a varying navig
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1fe765f9f5ada64cc89955b630df812b
https://doi.org/10.1177/0954410020930488
https://doi.org/10.1177/0954410020930488
Publikováno v:
IEEE Transactions on Aerospace and Electronic Systems. 55:236-250
This paper presents an impact time control guidance law that does not perform explicit time-to-go estimation. In order to satisfy the interception and the desired impact time constraint simultaneously, a sliding surface variable formulated as a sum o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::44fe1722b6664171f9657805ca79689d
https://doi.org/10.1109/taes.2018.2850208
https://doi.org/10.1109/taes.2018.2850208
Publikováno v:
IEEE Transactions on Aerospace and Electronic Systems. 52:671-680
An adaptive guidance law applicable to a short-range homing missile is investigated against a highly maneuvering target that has the same maximum maneuver acceleration as the missile. In practice, it is difficult to measure the target acceleration wi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::12b964c6f2f17a06b27811d4df781de6
https://doi.org/10.1109/taes.2015.140958
https://doi.org/10.1109/taes.2015.140958
Publikováno v:
IEEE Transactions on Aerospace and Electronic Systems. 52:938-947
This paper presents a blending principle of tail fins and reaction jets to achieve a fast response for a dual-controlled missile under a slew-rate limit. The blending principle can be categorized as controlling either the net force or the net moment
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b86a6ef4f116aa1a6a01c5de8d27eb35
https://doi.org/10.1109/taes.2015.140169
https://doi.org/10.1109/taes.2015.140169
Publikováno v:
Journal of Guidance, Control, and Dynamics. 39:61-68
A guidance problem for impact time control applicable to salvo attacks is considered based on the sliding mode control. To prevent the singularity of the guidance command, a positive continuous nonlinear function of the lead angle is introduced to th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3f85e9e26e21a29da7108389aabd9eb2
https://doi.org/10.2514/1.g001167
https://doi.org/10.2514/1.g001167
Publikováno v:
IEEE Transactions on Aerospace and Electronic Systems. 51:1310-1323
In this paper, a sliding mode guidance law for impact angle control is proposed against a maneuvering target with unknown acceleration, which is capable of achieving the acceptable miss distance and a wide range of the desired impact angle. The main
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::213d93957dbf07ae593a2fdefafe75fc
https://doi.org/10.1109/taes.2015.140358
https://doi.org/10.1109/taes.2015.140358
Publikováno v:
Mechatronics. 24:986-1000
In this paper, we present a control framework for the control of a hydraulic excavator. An excavator can be viewed as a robotic manipulator that interacts with the environment. It follows that the control method employed to control the excavator must
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2ede291b95bb38ff18ed818ff143f325
https://doi.org/10.1016/j.mechatronics.2014.10.004
https://doi.org/10.1016/j.mechatronics.2014.10.004
Publikováno v:
Autonomous Robots. 38:161-177
This paper investigates a decentralized trajectory optimization method to solve a nonlinear constrained trajectory optimization problem. Especially, we consider a problem constrained on the terminal time and angle in a multi-robot application. The pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b26ab2244663c90d4d198e278384d91e
https://doi.org/10.1007/s10514-014-9399-7
https://doi.org/10.1007/s10514-014-9399-7
Publikováno v:
2014 14th International Conference on Control, Automation and Systems (ICCAS 2014).
This paper presents an adaptive sliding mode control for a dual-controlled missile with tail fins and reaction jets. An RBF(Radial Basis Function) neural network is used to adaptively compensate for the uncertainties. The network adaptation rule is d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f0547587aab31e1b1b29ddad39038a3b
https://doi.org/10.1109/iccas.2014.6987751
https://doi.org/10.1109/iccas.2014.6987751
Autor:
H. Jin Kim, Dongsoo Cho
Publikováno v:
ACC
In this paper, an observer-based adaptive output feedback controller is developed for a class of strict-feedback nonlinear systems having unmatched uncertainties with unmeasured states. We transform an unmatched uncertain nonlinear system into the sy
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a679cb8e30bec09f391982d440bb28cd
https://doi.org/10.1109/acc.2013.6580658
https://doi.org/10.1109/acc.2013.6580658