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Hybrid verification of an interface for an automatic landing

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This paper appears in:
Decision and Control, 2002, Proceedings of the 41st IEEE Conference on
Date of Conference: 10-13 Dec. 2002
Author(s): Oishi, M.
Hybrid Syst. Lab., Stanford Univ., CA, USA
Mitchell, I. ;  Bayen, A. ;  Tomlin, C. ;  Degani, A.
Volume: 2
Page(s): 1607 - 1613 vol.2
Product Type: Conference Publications

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Abstract

Modern commercial aircraft have extensive automation which helps the pilot by performing computations, obtaining data, and completing procedural tasks. The pilot display must contain enough information so that the pilot can correctly predict the aircraft's behavior, while not overloading the pilot with unnecessary information. Human-automation interaction is currently evaluated through extensive simulation. In this paper, using both hybrid and discrete-event system techniques, we show how one could mathematically verify that an interface contains enough information for the pilot to safely and unambiguously complete a desired maneuver. We first develop a nonlinear, hybrid model for the longitudinal dynamics of a large civil jet aircraft in an autoland/go-around maneuver. We find the largest controlled subset of the aircraft's flight envelope for which we can guarantee both safe landing and safe go-around. We abstract a discrete procedural model using this result, and verify a discrete formulation of the pilot display against it. An interface which fails this verification could result in nondeterministic or unpredictable behavior from the pilot's point of view.

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