Zobrazeno 1 - 10
of 27
pro vyhledávání: '"Seong han Lee"'
Publikováno v:
International Journal of Aerospace Engineering, Vol 2021 (2021)
This study presents the unified high-fidelity flight dynamic modeling technique for compound aircraft. The existing flight dynamic modeling technique is absolutely depended on the experimental data measured by wind tunnel. It means that the existing
Externí odkaz:
https://doaj.org/article/dd2ce0c439ec4f50b4ca5a0328fa987a
Akademický článek
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Publikováno v:
Chinese Journal of Aeronautics. 34:6-19
This paper proposes a new direct method for an efficient trajectory optimization using the point that the dynamics of a deterministic system are uniquely determined by initial states and controls imposed over the time horizon of interest. To effectiv
Publikováno v:
International Journal of Control, Automation and Systems. 19:2634-2651
This paper proposes a new approach to the carrot-chasing guidance law to provide an accurate trajectory-tracking function. The ahead-distance approach used in the conventional method highly depends on trajectory shapes and the complex geometric manip
Publikováno v:
International Journal of Aerospace Engineering, Vol 2021 (2021)
This study presents the unified high-fidelity flight dynamic modeling technique for compound aircraft. The existing flight dynamic modeling technique is absolutely depended on the experimental data measured by wind tunnel. It means that the existing
Publikováno v:
International Journal of Aeronautical and Space Sciences. 22:648-662
This paper treats numerical methods for an efficient prediction of the rotorcraft emergency procedures after engine failures. The analytical means of compliance for the Category-A requirements can be used for the type certification of the transport-c
Publikováno v:
International Journal of Aeronautical and Space Sciences. 22:176-185
This paper intends to compare the effect of the attitude parameterization method on the performance of the attitude controller designed with the direct feedback of corresponding attitude states. To achieve this, the proportional-derivative controller
Publikováno v:
International Journal of Aeronautical and Space Sciences. 21:790-805
An inverse-simulation problem is reformulated to exactly satisfy the kinematic constraints imposed by the prescribed trajectory. Thereby, the problem can be transformed into an index 1 differential–algebraic equation that is much more easily solvab
Publikováno v:
Chinese Journal of Aeronautics, Vol 33, Iss 1, Pp 255-270 (2020)
This study creates and combines the general maneuver libraries for fixed-wing aircraft to implement tactical maneuvers. First, the generalized maneuver libraries are established by analyzing the characteristics of tactical maneuvers required in battl
Publikováno v:
Journal of Institute of Control, Robotics and Systems. 25:1048-1056