| dc.contributor.author | Jayarathne, Damsara | |
| dc.contributor.author | Paternain, Santiago | |
| dc.contributor.author | Mishra, Sandipan | |
| dc.date.accessioned | 2026-08-23T08:42:01Z | |
| dc.date.available | 2026-08-23T08:42:01Z | |
| dc.date.copyright | 2026/11/01 | |
| dc.date.issued | 2026 | |
| dc.identifier.issn | 0022-0434 | |
| dc.identifier.other | ds-25-1213.pdf | |
| dc.identifier.uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4316915 | |
| dc.description.abstract | Abstract. Helicopter aerial refueling is a particularly challenging maneuver because of the complex aerodynamic interaction between the helicopter, the hose–drogue, and the tanker. To address this, a control design and analysis framework for autonomous helicopter aerial refueling is presented here. The helicopter control architecture is based on standard inner and outer-loop cascaded dynamic inversion. The outer-loop dynamic-inversion-based control is augmented by a reinforcement learning (RL) controller that corrects the outer-loop commands to account for the unpredictable drogue motion. This RL corrective input and inner-loop tracking error result in imperfect dynamic inversion in the outer-loop, leading to a nonlinear residual term in the outer-loop dynamics. Hence, we derive analytical stability and performance bounds of the proposed controller in the presence of bounded drogue uncertainty, RL control actions, and imperfect inner-loop tracking. We then use these analytical expressions to design the model-based controller. Simulations in a high-fidelity environment with full-scale helicopter and drogue models validate the proposed method. These simulation results show that the proposed control strategy reduces the mean docking error from 0.26 m with the pure model-based controller to 0.08 m, demonstrating an improvement of 69% in docking error. Furthermore, the controller is shown to have a docking success rate of 88%, while adding additional disturbances from atmospheric turbulence, wind, and state uncertainty reduces the docking success rate to 70%. | |
| dc.publisher | The American Society of Mechanical Engineers (ASME) | |
| dc.title | Combining Model-Based Control and Reinforcement Learning for Autonomous Helicopter Aerial Refueling | |
| dc.type | Journal Paper | |
| dc.journal.volume | 148 | |
| dc.journal.issue | 6 | |
| dc.journal.title | Journal of Dynamic Systems, Measurement, and Control | |
| dc.identifier.doi | 10.1115/1.4071643 | |
| dc.journal.fristpage | 375 | |
| dc.journal.lastpage | 388 | |
| dc.page | 14 | |
| dc.tree | Journal of Dynamic Systems, Measurement, and Control:;2026:;volume( 148 ):;issue:006 | |
| dc.contenttype | Fulltext | |