A modeling methodology to facilitate safety-oriented architecture design of industrial avionics software
Summary Ensuring that avionics software meets safety requirements at each development stage is very important to warrant the safe operation of an avionics system. Many safety requirements are imposed by various standards and industrial regulations that must be met by avionics software. One of such s...
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| Vydáno v: | Software, practice & experience Ročník 45; číslo 7; s. 893 - 924 |
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Bognor Regis
Blackwell Publishing Ltd
01.07.2015
Wiley Subscription Services, Inc |
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| Abstract | Summary
Ensuring that avionics software meets safety requirements at each development stage is very important to warrant the safe operation of an avionics system. Many safety requirements are imposed by various standards and industrial regulations that must be met by avionics software. One of such standards is DO‐178B/C, which provides guidelines (e.g., development process and objectives to satisfy in development activities) for meeting safety requirements. This paper presents a modeling methodology including a UML profile for specifying safety requirements on a component‐based architecture model and a set of design guidelines on avionics software. These safety requirements were identified from both standards (mainly DO‐178B/C) and current engineering practices in the domain of avionics systems. The methodology automatically enforces these safety requirements. We have applied the methodology on an industrial autopilot system, and several previously uncaught faults were revealed. Copyright © 2014 John Wiley & Sons, Ltd. |
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| AbstractList | Ensuring that avionics software meets safety requirements at each development stage is very important to warrant the safe operation of an avionics system. Many safety requirements are imposed by various standards and industrial regulations that must be met by avionics software. One of such standards is DO‐178B/C, which provides guidelines (e.g., development process and objectives to satisfy in development activities) for meeting safety requirements. This paper presents a modeling methodology including a UML profile for specifying safety requirements on a component‐based architecture model and a set of design guidelines on avionics software. These safety requirements were identified from both standards (mainly DO‐178B/C) and current engineering practices in the domain of avionics systems. The methodology automatically enforces these safety requirements. We have applied the methodology on an industrial autopilot system, and several previously uncaught faults were revealed. Copyright © 2014 John Wiley & Sons, Ltd. Summary Ensuring that avionics software meets safety requirements at each development stage is very important to warrant the safe operation of an avionics system. Many safety requirements are imposed by various standards and industrial regulations that must be met by avionics software. One of such standards is DO-178B/C, which provides guidelines (e.g., development process and objectives to satisfy in development activities) for meeting safety requirements. This paper presents a modeling methodology including a UML profile for specifying safety requirements on a component-based architecture model and a set of design guidelines on avionics software. These safety requirements were identified from both standards (mainly DO-178B/C) and current engineering practices in the domain of avionics systems. The methodology automatically enforces these safety requirements. We have applied the methodology on an industrial autopilot system, and several previously uncaught faults were revealed. Copyright © 2014 John Wiley & Sons, Ltd. Ensuring that avionics software meets safety requirements at each development stage is very important to warrant the safe operation of an avionics system. Many safety requirements are imposed by various standards and industrial regulations that must be met by avionics software. One of such standards is DO-178B/C, which provides guidelines (e.g., development process and objectives to satisfy in development activities) for meeting safety requirements. This paper presents a modeling methodology including a UML profile for specifying safety requirements on a component-based architecture model and a set of design guidelines on avionics software. These safety requirements were identified from both standards (mainly DO-178B/C) and current engineering practices in the domain of avionics systems. The methodology automatically enforces these safety requirements. We have applied the methodology on an industrial autopilot system, and several previously uncaught faults were revealed. Summary Ensuring that avionics software meets safety requirements at each development stage is very important to warrant the safe operation of an avionics system. Many safety requirements are imposed by various standards and industrial regulations that must be met by avionics software. One of such standards is DO‐178B/C, which provides guidelines (e.g., development process and objectives to satisfy in development activities) for meeting safety requirements. This paper presents a modeling methodology including a UML profile for specifying safety requirements on a component‐based architecture model and a set of design guidelines on avionics software. These safety requirements were identified from both standards (mainly DO‐178B/C) and current engineering practices in the domain of avionics systems. The methodology automatically enforces these safety requirements. We have applied the methodology on an industrial autopilot system, and several previously uncaught faults were revealed. Copyright © 2014 John Wiley & Sons, Ltd. |
| Author | Yue, Tao Ali, Shaukat Wu, Ji Zhang, Huihui |
| Author_xml | – sequence: 1 givenname: Ji surname: Wu fullname: Wu, Ji email: Correspondence to: Ji Wu, School of Computer Science and Engineering, Beihang University, Beijing, China., wuji@buaa.edu.cn organization: State Key Laboratory of Software Development Environment, School of Computer Science and Engineering, Beihang University, Beijing, China – sequence: 2 givenname: Tao surname: Yue fullname: Yue, Tao organization: Certus Software Verification and Validation Center, Simula Research Laboratory, Lysaker, Norway – sequence: 3 givenname: Shaukat surname: Ali fullname: Ali, Shaukat organization: Certus Software Verification and Validation Center, Simula Research Laboratory, Lysaker, Norway – sequence: 4 givenname: Huihui surname: Zhang fullname: Zhang, Huihui organization: State Key Laboratory of Software Development Environment, School of Computer Science and Engineering, Beihang University, Beijing, China |
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| Notes | This paper is the extended version of the conference paper published in the 13th International Conference on Quality Software (QSIC 2013) [27]. This paper is sponsored jointly by State Key Laboratory of Software Development Environment (SKLSDE-2013ZX-12), Aeronautics Science Foundation of China (20121951021), Research Council of Norway under the Certus SFI project, and the Ministry of Industry and Trade of Norway, Ministry of Education of China under the Triple-One Program (grant number:B12025). istex:915FDE0803461658FDCEEEE4E139FD0D9219A538 ArticleID:SPE2281 ark:/67375/WNG-1VJX30V0-V th This paper is the extended version of the conference paper published in the 13 International Conference on Quality Software (QSIC 2013) [27]. This paper is sponsored jointly by State Key Laboratory of Software Development Environment (SKLSDE‐2013ZX‐12), Aeronautics Science Foundation of China (20121951021), Research Council of Norway under the Certus SFI project, and the Ministry of Industry and Trade of Norway, Ministry of Education of China under the Triple‐One Program (grant number:B12025). ObjectType-Article-1 SourceType-Scholarly Journals-1 ObjectType-Feature-2 content type line 14 content type line 23 |
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| References | Wiklander J, Eliasson J, Kruglyak A, et al. Enabling component-based design for embedded real-time software, Journal of Computers 2009; 4(12):1-34. Spitzer CR. Avionics: Elements, Software and Functions (Avionics Handbook). CRC Press: Florida, 2006. F De Florio, Airworthiness: An Introduction to Aircraft Certification, 2nd edition, Butterworth-Heinemann, 2011. Grunske L, Kaiser B, Reussner RH. Specification and Evaluation of Safety Properties in a Component-based Software Engineering Process, Chapter in Component-based Software Development for Embedded Systems: An Overview of Current Research Trends. Springer, 2005; 249-274. Baier C, Katoen J-P. Principles of Model Checking. MIT Press: Massachusetts, 2008. Hooman J, Kugler H, Ober I, et al. Supporting UML based development of embedded systems by formal techniques. Software and System Modeling 2008; 7(2):131-155. Wohlin C, Wesslen A. Experimentation in Software Engineering: An Introduction. Kluwer Academic Publishers; 2000. Berkenkotter K, Hannemann U. Modeling the Railway Control Domain Rigorously with a UML 2.0 Profile, SAFECOMP 2006. Springer: Heidelberg, 2006; 398-411. Bernardi S, Merseguer J, Petriu DC. A dependability profile within MARTE. Software System Model 2011; 10:313-336. Clarke E, McMillan K, Campos S, Hartonas-Garmhausen V. Symbolic model checking. Computer Aided Verification. Lecture Notes in Computer Science, 1996; 1102:419-422. Clarke EM, Emerson EA, Sistla AP. Automatic verification of finite-state concurrent systems using temporal logic specifications. ACM Transactions on Programming Languages and Systems. 8(2):244-263. 1986. 2001 2011 2000 1986; 8 2010 2007; 4735 1996; 1102 2008 2003; 58 1996 2008; 7 2007 2006 2011; 10 September 1991; 79 2005 2004 1982/2012 1981 2002 2009; 4 1978 e_1_2_9_30_1 e_1_2_9_31_1 e_1_2_9_11_1 e_1_2_9_34_1 e_1_2_9_10_1 e_1_2_9_35_1 e_1_2_9_13_1 e_1_2_9_32_1 e_1_2_9_33_1 Clarke EM (e_1_2_9_43_1) 1981 Baier C (e_1_2_9_12_1) 2008 Iqbal MZ (e_1_2_9_27_1) Clarke E (e_1_2_9_47_1) 1996; 1102 Berkenkotter K (e_1_2_9_6_1) 2006 e_1_2_9_15_1 e_1_2_9_38_1 e_1_2_9_14_1 e_1_2_9_39_1 e_1_2_9_17_1 e_1_2_9_16_1 e_1_2_9_37_1 e_1_2_9_19_1 e_1_2_9_18_1 e_1_2_9_41_1 Spitzer CR (e_1_2_9_2_1) 2006 e_1_2_9_42_1 e_1_2_9_20_1 e_1_2_9_40_1 e_1_2_9_45_1 e_1_2_9_21_1 e_1_2_9_46_1 e_1_2_9_24_1 e_1_2_9_23_1 e_1_2_9_44_1 e_1_2_9_8_1 e_1_2_9_7_1 e_1_2_9_5_1 e_1_2_9_4_1 e_1_2_9_3_1 e_1_2_9_9_1 e_1_2_9_26_1 De Florio F (e_1_2_9_22_1) 2011 e_1_2_9_25_1 NICHOLAS HALBWACHS, PAUL CASPI, PASCAL RAYMOND and DANIEL PILAUD (e_1_2_9_36_1) 1991 e_1_2_9_28_1 e_1_2_9_29_1 |
| References_xml | – reference: Spitzer CR. Avionics: Elements, Software and Functions (Avionics Handbook). CRC Press: Florida, 2006. – reference: Grunske L, Kaiser B, Reussner RH. Specification and Evaluation of Safety Properties in a Component-based Software Engineering Process, Chapter in Component-based Software Development for Embedded Systems: An Overview of Current Research Trends. Springer, 2005; 249-274. – reference: Baier C, Katoen J-P. Principles of Model Checking. MIT Press: Massachusetts, 2008. – reference: Wiklander J, Eliasson J, Kruglyak A, et al. Enabling component-based design for embedded real-time software, Journal of Computers 2009; 4(12):1-34. – reference: Clarke EM, Emerson EA, Sistla AP. Automatic verification of finite-state concurrent systems using temporal logic specifications. ACM Transactions on Programming Languages and Systems. 8(2):244-263. 1986. – reference: Wohlin C, Wesslen A. Experimentation in Software Engineering: An Introduction. Kluwer Academic Publishers; 2000. – reference: Berkenkotter K, Hannemann U. Modeling the Railway Control Domain Rigorously with a UML 2.0 Profile, SAFECOMP 2006. Springer: Heidelberg, 2006; 398-411. – reference: Hooman J, Kugler H, Ober I, et al. Supporting UML based development of embedded systems by formal techniques. Software and System Modeling 2008; 7(2):131-155. – reference: Clarke E, McMillan K, Campos S, Hartonas-Garmhausen V. Symbolic model checking. Computer Aided Verification. Lecture Notes in Computer Science, 1996; 1102:419-422. – reference: Bernardi S, Merseguer J, Petriu DC. A dependability profile within MARTE. Software System Model 2011; 10:313-336. – reference: F De Florio, Airworthiness: An Introduction to Aircraft Certification, 2nd edition, Butterworth-Heinemann, 2011. – year: 2011 – start-page: 236 year: 2011 end-page: 252 – volume: 8 start-page: 244 issue: 2 year: 1986 end-page: 263 article-title: Automatic verification of finite‐state concurrent systems using temporal logic specifications publication-title: ACM Transactions on Programming Languages and Systems – start-page: 642 end-page: 658 – year: 1981 – year: 2005 – start-page: 249 year: 2005 end-page: 274 – volume: 79 issue: 9 year: September 1991 – year: 2001 – year: 2007 – year: 1996 – year: 2000 – start-page: 55 end-page: 64 – year: 1982/2012 – year: 2010 – start-page: 201 year: 2010 end-page: 237 – volume: 1102 start-page: 419 year: 1996 end-page: 422 article-title: Symbolic model checking publication-title: Computer Aided Verification. 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| SubjectTerms | Architecture (computers) Avionics avionics software component-based architecture design Computer programs DO-178B/C Guidelines Methodology Safety Software UML profile |
| Title | A modeling methodology to facilitate safety-oriented architecture design of industrial avionics software |
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