DocumentCode :
238577
Title :
Mission critical software test philosophy a SILS based approach in Indian Mars Orbiter Mission
Author :
Sumith Shankar, S. ; Desai, K. ; Dutta, Suparna ; Chetwani, Rajiv R. ; Ravindra, M. ; Bharadwaj, K.M.
Author_Institution :
Satellite Centre, Software Quality Assurance Div., Syst. Reliability Group, ISRO, Bangalore, India
fYear :
2014
fDate :
27-29 Nov. 2014
Firstpage :
414
Lastpage :
419
Abstract :
ISRO Satellite Centre (ISAC) is the lead centre of the Indian Space Research Organisation in the development and operationalisation of satellites for communication, navigation and remote sensing applications. In all these spacecrafts, highly advanced embedded systems carryout variety of mission critical functions. Each of these embedded systems house heterogeneous Processor and Embedded Software Combinations to carry out their functionalities. As per existing practices, testing of on board software to confirm its functioning takes place only when the software is integrated with its associated hardware. On the contrary, by a technique called the Software in Loop Simulation (SILS) test method, the on-board software can be fully tested in a software simulated dynamic environment without Hardware. This method of flight software validation is demonstrated in MARS ORBITER MISSION for AOCE, TCP, SSR, BDH software. The results very well demonstrate the effectiveness of the technique in early performance prediction and assessment of on-board software. This validation philosophy will be followed for all future spacecrafts. In a development environment where software requirements are too complex and requirement changes are to be incorporated even during final stages of development, this technique offers an excellent solution in fully validating on board software at source code level before it gets integrated with target hardware. This additional validation step not only improves software quality but also enhances productivity and reduces system turnaround time.
Keywords :
aerospace computing; artificial satellites; embedded systems; program testing; program verification; satellite computers; software quality; AOCE software; BDH software; ISAC; ISRO Satellite Centre; Indian Mars Orbiter Mission; Indian Space Research Organisation; SILS based approach; SILS test method; SSR software; TCP software; communication application; embedded systems; flight software validation; heterogeneous processor-and-embedded software combination; mission critical functions; mission critical software test; navigation application; on-board software assessment; performance prediction; productivity enhancement; remote sensing application; satellite development; satellite operationalisation; software quality improvement; software requirements; software simulated dynamic environment; software-in-loop simulation test method; source code level; spacecrafts; system turnaround time reduction; target hardware; Informatics; Automation; Software In loop simulation; simulator; validation; verification;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Contemporary Computing and Informatics (IC3I), 2014 International Conference on
Conference_Location :
Mysore
Type :
conf
DOI :
10.1109/IC3I.2014.7019637
Filename :
7019637
Link To Document :
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