DocumentCode
3262716
Title
Hybrid verification of an interface for an automatic landing
Author
Oishi, Meeko ; Mitchell, Ian ; Bayen, Alexandre ; Tomlin, Claire ; Degani, Asaf
Author_Institution
Hybrid Syst. Lab., Stanford Univ., CA, USA
Volume
2
fYear
2002
fDate
10-13 Dec. 2002
Firstpage
1607
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.
Keywords
aerospace simulation; aircraft landing guidance; discrete event simulation; program verification; user interfaces; autoland/go-around maneuver; automatic landing; civil jet aircraft; commercial aircraft; discrete-event system techniques; flight envelope; human-automation interaction; hybrid interface verification; hybrid system techniques; longitudinal dynamics; nondeterministic behavior; nonlinear hybrid model; unpredictable behavior; Aerospace safety; Aircraft; Automatic control; Automation; Control systems; Displays; Humans; NASA; Software safety; State-space methods;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 2002, Proceedings of the 41st IEEE Conference on
ISSN
0191-2216
Print_ISBN
0-7803-7516-5
Type
conf
DOI
10.1109/CDC.2002.1184749
Filename
1184749
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