Zobrazeno 1 - 10
of 1 564
pro vyhledávání: '"dynamic inversion"'
Autor:
Marilena D. PAVEL
Publikováno v:
INCAS Bulletin, Vol 16, Iss 2, Pp 85-97 (2024)
Advanced nonlinear controllers are a desirable solution to rotorcraft flight control as they can solve the system high nonlinear dynamic behavior. However, conventional nonlinear controllers such as Nonlinear Dynamic Inversion (NDI) controller heavil
Externí odkaz:
https://doaj.org/article/13f5f1a80e634c5d8b43d0774370bbc2
Akademický článek
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Autor:
Lamsu Kim, Jeong I. Kim
Publikováno v:
Applied Sciences, Vol 14, Iss 22, p 10615 (2024)
A flight controller formulation based on incremental nonlinear dynamics inversion (INDI) control with nonlinear disturbance observer (NDO) is proposed. INDI control is a nonlinear controller based on incremental dynamics. Aimed to attain robustness f
Externí odkaz:
https://doaj.org/article/73655882093d45de85bf37c3e8514f63
Publikováno v:
Drones, Vol 8, Iss 10, p 599 (2024)
This study proposes a universal (U)-control enhanced with dynamic inversion for a class of multiple-input multiple-output (MIMO) quadrotor flight tracking operations. In the technique, a robust compensator is integrated with the U-controller to achie
Externí odkaz:
https://doaj.org/article/6b28a3f8ad73497585ab254e55f995c9
Publikováno v:
Actuators, Vol 13, Iss 6, p 227 (2024)
Considering the effect of icing on aircraft control performance, this paper proposes an adaptive dynamic inverse ice tolerance control method based on piecewise constant. A control allocation algorithm is introduced to compensate for the change of co
Externí odkaz:
https://doaj.org/article/316108a0724b480096a1ad604d588a10
Publikováno v:
Actuators, Vol 13, Iss 5, p 187 (2024)
Incremental nonlinear dynamic inversion (INDI) is a widely used approach to controlling UAVs with highly nonlinear dynamics. One key element of INDI-based controllers is the control allocation realizing pseudo controls using available actuators. Howe
Externí odkaz:
https://doaj.org/article/064e4ba2624a4b4cb1c355662c7c8c63
Publikováno v:
Drones, Vol 8, Iss 3, p 101 (2024)
This work investigates the pseudo-command restricted problem for tailless unmanned aerial vehicles with snake-shaped maneuver flight missions. The main challenge of designing such a pseudo-command restricted controller lies in the fact that the neces
Externí odkaz:
https://doaj.org/article/073102b010b943e48673e89bc0e9905c
Akademický článek
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Publikováno v:
IEEE Access, Vol 11, Pp 94805-94821 (2023)
This paper presents a real-time trajectory planning method for highly dynamic tracking control of wheeled inverted pendulum (WIP) systems. A generic form of dynamic inversion problem for the class of WIPs is defined by combining a set of kinematic an
Externí odkaz:
https://doaj.org/article/31ffdfc61c7444bbae3668d950239fc0
Publikováno v:
Aerospace, Vol 11, Iss 1, p 33 (2023)
A novel trajectory generation and control architecture for fully autonomous autorotative flare that combines rapid path generation with model-based control is proposed. The trajectory generation component uses optical Tau theory to compute flare traj
Externí odkaz:
https://doaj.org/article/ee17ec0a089b455b8e78ade70df8fcfe