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Requirements and Technical Concepts for Aviation Washington, DC: DO-178B: Software Considerations in Airborne Systems and Equipment Certiﬁcation, This document is known as EUROCAE ED-12B in Europe (December 1992) 4. : Applicability of modiﬁed condition/decision coverage to software testing. Issued for information under FAA memorandum ANM106N:93-20 (August 1993) 5. : A methodology for safety case development. pdf 6. UK Ministry of Defence: Interim Defence Standard 00-56, Issue 3: Safety Management Requirements for Defence Systems.
RV 2007. LNCS, vol. 4839, pp. 111–125. Springer, Heidelberg (2007) 15. php/Monitoring-Oriented Programming 16. Australian Transport Safety Bureau: In-ﬂight upset event, 240 km northwest of Perth, WA, Boeing Company 777-200, 9M-MRG, Reference number Mar2007/DOTARS 50165. aspx. aspx 17. : An intrusion-detection model. IEEE Transactions on Software Engineering 13(2), 222–232 (1987) 18. : Intrusion detection via static analysis. In: Proceedings of the Symposium on Security and Privacy, pp. 156–168.
In more complicated cases, the controller must really be a strategy that reacts to the environment rather than a simple sequence or a schedule. In this situation, the controller synthesis problem can be solved using techniques derived from model checking . The advantage of a formal, model-based approach to mitigation is that it can consider multiple possible diagnoses and calculate the best overall response. The model can also be cognizant of system-level safety properties, so that we can be sure that an action that seems reasonable at the local level does not have adverse consequences at a higher level (as in the case of American Flight 903).