TY - GEN
T1 - Modeling and Analysis of Collision Avoidance with ACAS Xu in Verse for the GUAM Lift + Cruise Model
AU - Bullock, John L.
AU - Song, Lin
AU - Puthumanaillam, Gokul
AU - Li, Yangge
AU - Cheng, Sheng
AU - Ornik, Melkior
AU - Mitra, Sayan
AU - Hovakimyan, Naira
N1 - This work is supported by NASA cooperative agreement (80NSSC20M0229), NASA ULI (80NSSC22M0070), AFOSR (FA9550-21-1-0411), and NSF-AoF Robust Intelligence (2133656). We thank both Oswin So and Chuchu Fan (MIT) for their development of the Python-based GUAM simulation. We also thank the Intelligent Contingency Management group at NASA Langley Research Center for developing the original GUAM simulator and their subsequent insightful discussions.
PY - 2025
Y1 - 2025
N2 - As advanced air mobility technology matures and becomes widely adopted, urban environments are expected to experience a high density of air traffic. To improve operational safety in dense traffic scenarios, collision avoidance protocols can be implemented in these air vehicles to generate high-level command advisories to avoid nearby vehicles or obstacles. Toward this end, some collision avoidance controllers have been implemented as data-driven modules, such as neural networks, to replace advisory lookup tables for storage and computational efficiency gains. However, small perturbations to the input of the neural network can potentially lead to different advisory outputs. Hence, neural network controllers must be verified to produce safe command advisories, which are then propagated through the vehicle dynamics for closed-loop verification purposes. In this work, we propose a framework for modeling and simulating a Lift+Cruise vehicle guided by collision avoidance advisories. The collision avoidance advisories are generated by a decision tree that approximates the existing ACAS Xu neural network system. The simulation is implemented in the Verse library to propagate the collision avoidance commands through the nonlinear Lift+Cruise vehicle dynamics in a closed-loop manner. This approach is used to generate simulations from a variety of initial vehicle conditions to find scenarios where ACAS Xu advisories can potentially lead to near mid-air collisions.
AB - As advanced air mobility technology matures and becomes widely adopted, urban environments are expected to experience a high density of air traffic. To improve operational safety in dense traffic scenarios, collision avoidance protocols can be implemented in these air vehicles to generate high-level command advisories to avoid nearby vehicles or obstacles. Toward this end, some collision avoidance controllers have been implemented as data-driven modules, such as neural networks, to replace advisory lookup tables for storage and computational efficiency gains. However, small perturbations to the input of the neural network can potentially lead to different advisory outputs. Hence, neural network controllers must be verified to produce safe command advisories, which are then propagated through the vehicle dynamics for closed-loop verification purposes. In this work, we propose a framework for modeling and simulating a Lift+Cruise vehicle guided by collision avoidance advisories. The collision avoidance advisories are generated by a decision tree that approximates the existing ACAS Xu neural network system. The simulation is implemented in the Verse library to propagate the collision avoidance commands through the nonlinear Lift+Cruise vehicle dynamics in a closed-loop manner. This approach is used to generate simulations from a variety of initial vehicle conditions to find scenarios where ACAS Xu advisories can potentially lead to near mid-air collisions.
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U2 - 10.2514/6.2025-1323
DO - 10.2514/6.2025-1323
M3 - Conference contribution
AN - SCOPUS:86000031290
SN - 9781624107238
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
BT - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
Y2 - 6 January 2025 through 10 January 2025
ER -