Technology needs for development of the ultra long life missions
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Engineering topics
Publications and source records attributed to Chau, S..
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In this paper, we present a performability study that analyzes the guarded operation duration for onboard software upgrading.
We propose a new conceptual approach to system-level autonomy that exploits in a synergistic way recent breakthroughs in three specific areas: automatic generation of embeddable planning and validation software, integration of telecommunications forecaster and planning tools, and fault-tolerant assignment of computing tasks to multiple processors.
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In order to shorten the avionics architecture development time, the Jet Propulsion Laboratory has developed a model-based architecture simultion tool called the Avionics System Architecture Tool (ASAT).
In this paper I will briefly describe JPL's history and some major discoveries we've made in deep space exploration.
In preparing for the space exploration challenges of the next century, the national aeronautics and space administration (NASA) center for integrated space micro-systems (CISM) is chartered to develop advanced spacecraft systems that can be adapted for a large spectrum of future space missions.
This paper summarizes work in progress in three different areas: 1) a framework for the design of higly reliable and higly available space avionics systems; 2) distributed reliable computing architecture; and 3) Guarded Software Upgrading (GSU) techniques for software upgrading during long-term missions such as the Pluto/Kuiper missions.
The design of highly survivable avionics systems for long-term (> 10 years) exploration of space is an essential technology for all current and future missions in the Outer Planets roadmap. Long-term exposure to extreme environmental conditions such as high radiation and low-temperatures make survivability in space a major challenge. Moreover, current and future missions are increasingly using commercial technology such as deep sub-micron (0.25 microns) fabrication processes with specialized circuit designs, commercial interfaces, processors, memory, and other commercial off the shelf components that were not designed for long-term survivability in space. Therefore, the design of highly reliable, and available systems for the exploration of Europa, Pluto and other destinations in deep-space require a comprehensive and fresh approach to this problem. This paper summarizes work in progress in three different areas: a framework for the design of highly reliable and highly available space avionics systems, distributed reliable computing architecture, and Guarded Software Upgrading (GSU) techniques for software upgrading during long-term missions. Additional information is contained in the original extended abstract.
Information and discussion of the development of an Avionics Architecture Tool that is model-based using commercial off the shelf (COTS) products will be provided.
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Fault-tolerant systems are traditionally divided into fault containment regions and custom logic is added to ensure the effects of a fault within a containment region would not propagate to the other regions.
In order to accomplish dependable onboard evolution, we develop a methodology which is called guarded software upgrading (GSU).
In this paper, we report our experiences and findings on the design of fault-tolerant bus architecture comprised of two COT buses, the IEEE 1394 and the I***Sup 2***C.
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Using COTS products, standards and intellectual properties (IPs) for all the system and component interfaces is a crucial step toward significant reduction of both system cost and development cost, as the COTS interfaces enable other COTS products and IPs to be readily accommodated by the target system architecture.