TY - GEN
T1 - Dynamic Collision-Inclusive Modeling of a Multirotor Aerial Vehicle using Linear Complementarity Systems
AU - Abazari, Amirali
AU - Kumar, Yogesh
AU - Patnaik, Karishma
AU - Zhang, Wenlong
N1 - Publisher Copyright: © 2025 AACC.
PY - 2025
Y1 - 2025
N2 - Fast and discontinuous nature of collision has raised many challenges in modeling and control of mobile robots, especially for those with agile dynamics such as multi-rotor Micro Aerial Vehicles (MAVs). In this paper, a Linear Complementarity System (LCS) model is developed to model collisions between a multirotor MAV and the surrounding environment. The contact properties and model parameters are obtained by minimizing the error between the simulation and the experimental data. The derived collision model is then verified through a series of collision experiments using a custom-designed setup. Simulation results show that the developed model is capable of estimating the post-collision velocity with the average error lower than 0.1 m/s (for maximum collision velocity of 0.91 m/s and rebound velocity of 0.4 m/s) and the maximum normal contact force errors as low as 0.25 N (≤1% of the maximum normal force).
AB - Fast and discontinuous nature of collision has raised many challenges in modeling and control of mobile robots, especially for those with agile dynamics such as multi-rotor Micro Aerial Vehicles (MAVs). In this paper, a Linear Complementarity System (LCS) model is developed to model collisions between a multirotor MAV and the surrounding environment. The contact properties and model parameters are obtained by minimizing the error between the simulation and the experimental data. The derived collision model is then verified through a series of collision experiments using a custom-designed setup. Simulation results show that the developed model is capable of estimating the post-collision velocity with the average error lower than 0.1 m/s (for maximum collision velocity of 0.91 m/s and rebound velocity of 0.4 m/s) and the maximum normal contact force errors as low as 0.25 N (≤1% of the maximum normal force).
UR - https://www.scopus.com/pages/publications/105015786911
UR - https://www.scopus.com/pages/publications/105015786911#tab=citedBy
U2 - 10.23919/ACC63710.2025.11107858
DO - 10.23919/ACC63710.2025.11107858
M3 - Conference contribution
T3 - Proceedings of the American Control Conference
SP - 5135
EP - 5141
BT - 2025 American Control Conference, ACC 2025
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2025 American Control Conference, ACC 2025
Y2 - 8 July 2025 through 10 July 2025
ER -