V4.5

Final version of Safety models (functional and physical) and documents
associated to System version V4.5

models/SimfiaNeoproject - physical model/AIDA_V4_5_physical/.project

@@ -0,0 +1,12 @@
+<?xml version="1.0" encoding="UTF-8"?>
+<projectDescription>
+	<name>AIDA_V4_5_physical</name>
+	<comment></comment>
+	<projects>
+	</projects>
+	<buildSpec>
+	</buildSpec>
+	<natures>
+		<nature>org.eclipse.sirius.nature.modelingproject</nature>
+	</natures>
+</projectDescription>

readme.txt

@@ -29,7 +29,7 @@ The quadcopter drone can be piloted in automated or manual mode. In manual mode,
 the pilot guides the inspection of the aircraft by the drone. 
 In automated mode, the drone follows a flight plan and records the video of the inspected zone.
 
-Corresponding SE version (see AIDA Architecture repository): V4.4 - S2C MS3 delivery
+Corresponding SE version (see AIDA Architecture repository): V4.5 - S2C final delivery
 
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 * 2. Motivation and intended use
@@ -50,15 +50,21 @@ https://doi.org/10.1007/978-3-319-64119-5_2
 * 3. List of files and how to use them
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-- model : contains the SimfiaNeo model (to be opened with SimfiaNeo V1.3.2 - see https://www.protect.airbus.com/safe-mobility/simfianeo/ for more information)
+- model : contains the SimfiaNeo models (to be opened with SimfiaNeo V1.4.2 - see https://www.protect.airbus.com/safe-mobility/simfianeo/ for more information)
+	- functional model : an MBSA model based on the functional architecture of AIDA.
+	- physical model : an MBSA model based on the physical architecture of AIDA.
 	
-- documents : contains the safety documents created and/or used for the SE-SA process illustration (see deliverable ISX-S2C-LIV-1235 of S2C project): 
-	- FHA AIDA V4.4 : Aircraft level FHA
-	- PASA - FTA : ault trees for CAT and HAZ failure conditions, for system level requirements definition (PASA)
-	- PASA AIDA V4.4 : synthesis of requirements for system level
-	- SFHA : System FHA, covering all the systems of AIDA
-	- Propulsion system FMES-SFMEA : FMES and SFMEA at item levels for the constituant of the propulsion system
-	- SSA propulsion system : compliance of propulsion system to the requirements established in PASA
+- documents : contains the safety documents related to the AIDA use case, inspired from ARP4754A and ARP4761 guidelines:
+	- AIDA - SORA analysis : partial SORA analysis of the AIDA concepts, as proposed by EASA for Unmanned Aircraft Systems operations in Specific category (see https://www.easa.europa.eu/en/document-library/easy-access-rules/easy-access-rules-unmanned-aircraft-systems-regulations-eu) 
+	- Aircraft level folder : safety documents related to the "Aircraft level" 
+		- FHA AIDA: Aircraft level FHA
+		- PASA - FTA : ault trees for CAT and HAZ failure conditions, for system level requirements definition (PASA)
+		- PASA AIDA : synthesis of requirements for system level
+	- System level folder : safety documents related to the "System level"
+		- SFHA AIDA: System FHA, covering all the systems of AIDA
+		- PSSA AIDA : PSSA analysis, exploiting the computation results of the MBSA physical model, and establishing the requirements for the Item levels
+		- FMES-SFMEA : simulated FMES and SFMEA at item levels for all the constituant of AIDA
+		- SSA : compliance of AIDA to the top-level requirements, integrating the quantitative results contained in the SFMEA.
 
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 * 4. Licensing information