DocumentCode
43970
Title
High Confidence Networked Control for Next Generation Air Transportation Systems
Author
Park, Pyeongyeol ; Khadilkar, Harshad ; Balakrishnan, H. ; Tomlin, Claire J.
Author_Institution
Dept. of Electr. Eng. & Comput. Sci., Univ. of California at Berkeley, Berkeley, CA, USA
Volume
59
Issue
12
fYear
2014
fDate
Dec. 2014
Firstpage
3357
Lastpage
3372
Abstract
This paper addresses the design of a secure and fault-tolerant air transportation system in the presence of attempts to disrupt the system through the satellite-based navigation system. Adversarial aircraft are assumed to transmit incorrect position and intent information, potentially leading to violations of separation requirements among aircraft. We propose a framework for the identification of adversaries and malicious aircraft, and then for air traffic control in the presence of such deliberately erroneous data. The framework consists of three mechanisms that allow each aircraft to detect attacks and to resolve conflicts: fault detection and defense techniques to improve Global Positioning System (GPS)/inertial navigation, detection and defense techniques using the Doppler/received signal strength, and a fault-tolerant control algorithm. A Kalman filter is used to fuse high frequency inertial sensor information with low frequency GPS data. To verify aircraft position through GPS/inertial navigation, we propose a technique for aircraft localization utilizing the Doppler effect and received signal strength from neighboring aircraft. The control algorithm is designed to minimize flight times while meeting safety constraints. Additional separation is introduced to compensate for the uncertainty of surveillance information in the presence of adversaries. We evaluate the effect of air traffic surveillance attacks on system performance through simulations. The results show that the proposed mechanism robustly detects and corrects faults generated by the injection of malicious data. Moreover, the proposed control algorithm continuously adapts operations in order to mitigate the effects these faults. The ability of the proposed approaches to defend against attacks enables reliable air traffic operations even in highly adversarial surveillance conditions.
Keywords
Doppler effect; Global Positioning System; Kalman filters; aerospace safety; air traffic control; aircraft control; aircraft navigation; fault tolerant control; inertial navigation; networked control systems; position control; signal processing; surveillance; Doppler effect; Global Positioning System; Kalman filter; adversarial aircraft; adversaries identification; air traffic control; air traffic operations; air traffic surveillance attacks; aircraft localization; aircraft position; attacks detection; defense techniques; design; detection techniques; fault detection; fault-tolerant air transportation system; fault-tolerant control algorithm; flight times minimization; high confidence networked control; high frequency inertial sensor information; inertial navigation; low frequency GPS data; malicious aircraft; next generation air transportation systems; received signal strength; safety constraints; satellite-based navigation system; secure air transportation system; surveillance information; system performance; Aerospace control; Aircraft; Aircraft navigation; Atmospheric modeling; Doppler effect; Global Positioning System; Surveillance; Automatic dependent surveillance???Broadcast; intelligent control; misbehavior detection; next generation air transportation systems;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/TAC.2014.2352011
Filename
6882825
Link To Document