This paper presents a learning-based adaptive augmentation control concept inspired by the adaptation mechanisms of conventional adaptive control, while not being restricted to their specific parametric adaptation structures. In contrast to augmenting a reinforcement learning (RL) baseline controller with classical adaptive control to account for the simulation-to-reality gap, the proposed approach uses RL-based adaptive augmentation to address the limitations of conventional adaptive control. Domain randomization combined with observation stacking is employed to train the RL-based augmentation to compensate for matched uncertainties in a fixed-wing aircraft system. To ensure constraint satisfaction during operation, a safety filter is incorporated into the control architecture. Based on the concept of pseudo control hedging (PCH), we propose a modified reference model that avoids undesirable interactions between the RL-based augmentation and the safety filter. To reduce the conservatism of the safety filter, we additionally incorporate a disturbance observer. The proposed approach is evaluated on a fixed-wing aircraft model subject to uncertainties.
Traditional Proportional–Integral–Derivative (PID) controllers are the dominant solution for Unmanned Aerial Vehicle (UAV) attitude stabilization due to their simplicity and low computational cost. However, their fixed tuning parameters limit performance under nonlinear dynamics, rapidly varying flight conditions, and...
I. Laabousse, Y. El Bouzekri El Idrissi, Mohamed Haidoury et al.· Engineering, Technology &...· 0 citations
Robust tracking under nonlinear uncertainty and actuator constraints remains challenging for model-reference adaptive control (MRAC). Deep reinforcement learning (RL) can compensate for nonlinear effects, but a standalone policy provides no inherent model-reference structure. This paper combines an MRAC backbone with a...
Abdelrehim A. Elembaby, B. Emran· IEEE Access· 0 citations
To address issues such as nonlinear strong coupling, time-varying parameters, and external wind disturbances in fixed-wing unmanned aerial vehicles (UAVs) operating in complex flight environments, this study develops a composite attitude control method integrating L1 adaptive control with an extended state observer (ES...
Cheng Chen, Wen-Xi Tu, Yang Liu et al.· Actuators· 0 citations
This paper presents a learning-enhanced nonlinear model predictive control approach for 3-D path-following guidance of a fixed-wing small uncrewed aircraft system along with flight test evaluation. A generic framework is introduced that leverages learned meta-level policies for dynamically adjusting inputs to an underl...
C. A. Hirst, Chris Reale, E. Frew· Journal of Guidance Control...· 1 citation
This research introduces an innovative control technique for Series Elastic Actuators (SEAs) that utilizes Reinforcement Learning (RL) to address the shortcomings of previously fixed-gain adaptive controllers, which are a hybrid of State Feedback Control and Model Reference Adaptive Control by using Lyapunov Stability...
H. Z. Abdalikhwa, Waleed Al-Ashtari· International journal of com...· 0 citations
Trajectory tracking for flapping-wing microaerial vehicles (FWMAVs) is challenging due to inherent nonlinear dynamics and unsteady aerodynamics. While incremental model predictive control (IMPC) effectively manages constraints, its reliance on fixed weighting matrices limits performance during aggressive maneuvers. Con...
Zhong-Qi Lu, Zhi-Jie Liu, Hang Zhong et al.· IEEE Transactions on Neural...· 0 citations
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