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 :
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