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• |
Inputs
from environment
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– |
Altitude
:= {1000…8000}
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• |
Simplification
of functions
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– |
Alt_Rate
:=
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0.25*(Alt_Baro-ZP)/Delta_t
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– |
Alt_Rate
:= {-2000…2000}
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• |
Unmodelled
parts of specification
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– |
States
of Other_Aircraft treated as non-
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deterministic
input variables
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