Abstract

Adaptive Navigation (AN) control strategies allow an agent to autonomously alter its trajectory based on realtime measurements of the environment. Compared to conventional navigation methods, these techniques can reduce required time and energy to explore scalar characteristics of unknown and dynamic regions of interest (e.g., temperature, concentration level). Multiple Uncrewed Aerial Vehicle (UAV) approaches to AN can improve performance by exploiting synchronized spatially-dispersed measurements to generate realtime information regarding the structure of the local scalar field, which is then used to inform navigation decisions. This article presents initial results of a comprehensive program to develop, verify, and experimentally implement mission-level AN capabilities in three-dimensional (3D) space using our unique multilayer control architecture for groups of vehicles. Using our flexible formation control system, we build upon our prior 2D AN work and provide new contributions to 3D scalar field AN by a) demonstrating a wide range of 3D AN capabilities using a unified, multilayer control architecture, b) extending multivehicle 2D AN control primitives to navigation in 3D scalar fields, and c) introducing state-based sequencing of these primitive AN functions to execute 3D mission-level capabilities such as isosurface mapping and plume following. We verify functionality using high-fidelity simulations of multicopter drone clusters, accounting for vehicle dynamics, outdoor wind gust disturbances, position sensor inaccuracy, and scalar field sensor noise. This paper presents the multilayer architecture for multivehicle formation control, the 3D AN control primitives, the sequencing approaches for specific mission-level capabilities, and simulation results that demonstrate these functions.

Highlights

  • Conventional navigation techniques involve user-provided waypoints or a predefined trajectory for an agent to follow over time

  • Description Cluster point B position vector P⃗B projected onto Gn Desired scalar value of isosurface Mean of scalar field measurements Scalar field threshold for isosurface Plume following start threshold Plume following end threshold Distance between map start / end Angle between map start / end Angle between ggrad and Gn Differentials magnitude threshold Cluster alignment threshold Cluster rotational gain

  • Experiments have been performed with UAVs at fixed altitudes in small indoor testbeds. [35] implemented gradientbased control of three DJI Flamewheel 450 UAVs in fixed circular formations to demonstrate moving light source seeking and three Crazyflie 2.0 UAVs to perform level set tracking/tracing about a simulated scalar field in a small enclosed area ~2 m2. [73] used seven Crazyflie 2.1 UAVs at fixed altitudes to swarm towards simulated scalar field sources in a region ~12 m2

Read more

Summary

Introduction

Conventional navigation techniques involve user-provided waypoints or a predefined trajectory for an agent to follow over time. Adaptive Navigation (AN) methods allow an agent to autonomously alter its trajectory or direction based on realtime measurements of the environment. The most basic form of adaptive navigation requires specifying the destination explicitly while allowing the control system to alter the vehicle’s path, such as rerouting to avoid obstacles or traffic congestion. More advanced AN systems do not require user specified destinations in any form such as enemy evasion while being pursued or autonomously determining the optimal escape route. Scalar field features represent significant phenomena in a wide range of applications such as environmental monitoring/characterization, disaster response, and exploration. A detailed discussion of scalar field features is TABLE I

Methods
Findings
Discussion
Conclusion
Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call