Modeling and switching adaptive control for nonlinear morphing aircraft considering actuator dynamics
W Xu, Y Li, M Lv, B Pei - Aerospace Science and Technology, 2022 - Elsevier
This paper investigates the problems of modeling and control of the morphing aircraft.
Henceforth, a nonlinear dynamic model of a wing-sweep morphing aircraft is first …
Henceforth, a nonlinear dynamic model of a wing-sweep morphing aircraft is first …
[HTML][HTML] A review of control strategies used for morphing aircraft applications
MS Parancheerivilakkathil, JS Pilakkadan… - Chinese Journal of …, 2024 - Elsevier
This paper reviews the various control algorithms and strategies used for fixed-wing
morphing aircraft applications. It is evident from the literature that the development of control …
morphing aircraft applications. It is evident from the literature that the development of control …
[PDF][PDF] A review of control strategies used for morphing aircraft applications
SP Muhammed, SP Jafar, M Rafic… - Chin. J …, 2023 - researchgate.net
This paper reviews the various control algorithms and strategies used for fixed-wing
morphing aircraft applications. It is evident from the literature that the development of control …
morphing aircraft applications. It is evident from the literature that the development of control …
Flight dynamics modeling and stability analysis of a tube-launched tandem wing aerial vehicle during the deploying process
H Cheng, Q Shi, H Wang, W Shan… - Proceedings of the …, 2022 - journals.sagepub.com
During the subsequent deploying process after the launch, the vehicle experiences dramatic
changes in geometry as well as aerodynamics, which cannot be ignored for the flight …
changes in geometry as well as aerodynamics, which cannot be ignored for the flight …
Linear parameter-varying control of variable span-sweep morphing aircraft
An aircraft capable of large-scale in-flight shape changes is called a morphing aircraft.
According to a given mission and flight condition, the shape of the morphing aircraft is …
According to a given mission and flight condition, the shape of the morphing aircraft is …
Recurrent neural network-based predefined time control for morphing aircraft with asymmetric time-varying constraints
J Pu, Y Zhang, Y Guan, N Cui - Applied Mathematical Modelling, 2024 - Elsevier
This paper proposes a predefined time control method for morphing aircraft based on an
adaptive full-feedback recurrent neural network and a universal barrier function. This …
adaptive full-feedback recurrent neural network and a universal barrier function. This …
Honeycomb structure filling morphing wing trailing edge: Design strategy, deformation feedback, and active control
X Li, L Sun, Y Pan, X Guo - Programmable Materials, 2024 - cambridge.org
Pursuing highly efficient aerodynamic efficiency in aircraft has driven the development of
morphing wing technology. However, there are still limitations to morphing wing technology …
morphing wing technology. However, there are still limitations to morphing wing technology …
Dynamics Modeling and Autonomous Landing for Flexible Parafoil-Vehicle Multibody System
L Yan, Y Song, H Wang, Z Shi - IEEE Access, 2023 - ieeexplore.ieee.org
In this paper, the autonomous landing of the parafoil used for aerial vehicles is investigated
through the numerical approach. The coupled parafoil-vehicle dynamics model is developed …
through the numerical approach. The coupled parafoil-vehicle dynamics model is developed …
A Generative Verification Framework on Statistical Stability for Data-Driven Controllers
S Lee - IEEE Access, 2023 - ieeexplore.ieee.org
This study proposes a novel framework for evaluating the stability of data-driven controllers
and the concept of statistical stability. The proposed framework can be used when it is …
and the concept of statistical stability. The proposed framework can be used when it is …
Actor-critic-based optimal adaptive control design for morphing aircraft
An online actor-critic-based control design strategy is proposed for a variable span and
sweep morphing wing aircraft considering the morphing parameters as control effectors …
sweep morphing wing aircraft considering the morphing parameters as control effectors …