Issues in Design and Development of Reliable Configurable Distributed Checkout and Launch System for Mission Critical Aero-Space Flight Vehicles
Shivpal Singh1, Bhogendra Rao PVRR2
1Shivpal Singh, M.Tech, Department of Computer Science, IIT, Madras India.
2Dr. PVRR Bhogendra Rao, Ph.D, Department of Computer Science, JNTU, Hyderabad (Telangana), India.
Manuscript received on 25 February 2020 | Revised Manuscript received on 05 March 2020 | Manuscript Published on 15 March 2020 | PP: 77-81 | Volume-9 Issue-4S2 March 2020 | Retrieval Number: D10180394S220/2020©BEIESP | DOI: 10.35940/ijitee.D1018.0394S220
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© The Authors. Blue Eyes Intelligence Engineering and Sciences Publication (BEIESP). This is an open-access article under the CC-BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/)
Abstract: Role of Configurable Distributed Checkout and Launch System (CDCLS) is pivotal in carrying out quick health checks and launching of Aerospace Flight Vehicles. Configurable Distributed Architecture provides flexibility for connecting nodes and scaling Distributed System. Different configurations can be derived from the Master Configuration. Since, Ultra high reliability and infallible performance of the CDCLS is of paramount importance, Safety criticality and Mission criticality analysis needs to be carried out for determination of mission critical parameters. These critical parameters need to be addressed by required fault tolerant architecture, which can be implemented in Hardware and Software for achieving system reliability objective (Say, 0.99).
Keywords: Distributed System, Launch System, Reliability, Fault Tolerance, Automated Testing, System Validation.
Scope of the Article: Optical Link Design