scholarly journals Dynamic Mission Planning for Communication Control in Multiple Unmanned Aircraft Teams

2013 ◽  
Vol 01 (01) ◽  
pp. 41-58 ◽  
Author(s):  
Andrew N. Kopeikin ◽  
Sameera S. Ponda ◽  
Luke B. Johnson ◽  
Jonathan P. How

A multi-UAV system relies on communications to operate. Failure to communicate remotely sensed mission data to the base may render the system ineffective, and the inability to exchange command and control messages can lead to system failures. This paper describes a unique method to control network communications through distributed task allocation to engage under-utilized UAVs to serve as communication relays and to ensure that the network supports mission tasks. This work builds upon a distributed algorithm previously developed by the authors, CBBA with Relays, which uses task assignment information, including task location and proposed execution time, to predict the network topology and plan support using relays. By explicitly coupling task assignment and relay creation processes, the team is able to optimize the use of agents to address the needs of dynamic complex missions. In this work, the algorithm is extended to explicitly consider realistic network communication dynamics, including path loss, stochastic fading, and information routing. Simulation and flight test results validate the proposed approach, demonstrating that the algorithm ensures both data-rate and interconnectivity bit-error-rate requirements during task execution.

2004 ◽  
Vol 27 (6) ◽  
pp. 975-988 ◽  
Author(s):  
John D. Schierman ◽  
David G. Ward ◽  
Jason R. Hull ◽  
Neha Gandhi ◽  
Michael Oppenheimer ◽  
...  

2022 ◽  
Author(s):  
James L. Gresham ◽  
Jean-Michel W. Fahmi ◽  
Benjamin M. Simmons ◽  
Jeremy W. Hopwood ◽  
Wade Foster ◽  
...  

2017 ◽  
Vol 2017 (2) ◽  
pp. 80-96
Author(s):  
Marcin Żugaj

Abstract Reliability of unmanned aircraft is a decisive factor for conducting air tasks in controlled airspace. One of the means used to improve unmanned aircraft reliability is reconfiguration of the control system, which will allow to maintain control over the aircraft despite occurring failures. The control system is reconfigured by using operational control surfaces, to compensate for failure consequences and to control the damaged aircraft. Development of effective reconfiguration algorithms involves utilization of a non-linear model of unmanned aircraft dynamics, in which deflection of each control surface can be controlled independently. The paper presents a method for an unmanned aircraft control system reconfiguration utilizing a linear and nonlinear model of aerodynamic loads due to control. It presents reconfiguration algorithms, which differ with used models and with optimization criteria for deflections of failure-free control surfaces. Additionally it presents results of a benchmark of the developed algorithms, for various types of control system failures and control input.


Sign in / Sign up

Export Citation Format

Share Document