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Overview
This book discusses .the use of microprocessors in space missions, from the earliest 4-bit machines to the most current 32-bit implementations. It covers the transition from monolithic processors with extensive glue logic, to IP cores instantiated in FPGA's. It gives the high-lights of the microprocessors sent and being sent into space, and the problems of sustaining their operations there. Microprocessors orbit the earth, sit on other planets, and have left the Solar system into interstellar space. They are the key components for spacecraft autonomy, and for collecting, storing, and returning the volumes of information that we receive from off-planet sources.
Spacecraft microprocessors are a special subset of embedded computers. Most spacecraft include 10's ro 100's of processors, doing tasks such as attitude and orbit control, power monitoring and control, telemetry formatting and command handling, data storage management, and instrument control. Without these microprocessors, the amount that we know about our neighboring planets and the intervening space would be vastly limited.
Early flight computers were custom designs, but cost and performance issues have driven the development of variants of commercial chips. Aerospace applications are usually classic embedded applications. Space applications are rather limited in number, and, until recently, almost exclusively meant NASA, ESA, or some other government agency. Flight systems electronics usually require MIL-STD-883b, Class-S, radiation-hard (total dose), SEU-tolerant parts. Specific issues of radiation tolerance are disucssed. Class-S parts are specifically for space-flight use. Because of the need for qualifying the parts for space, the state-of-the-art in spaceborne electronics usually lags that of the terrestrial commercial parts by 5 years.
Processors used in aerospace applications, as any semiconductor-based electronics, need to meet stringent selection, screening, packaging and testing requirements, and characterizations because of the unique environment. Most aerospace electronics, and the whole understanding of radiation effects, were driven by the cold war defense buildup from the 1960's through the 1980's. This era was characterized by the function-at-any-cost, melt-before-fail design philosophy. In the 1990, the byword was COTS -- use of Commercial, Off-The-Shelf products. Thus, instead of custom, proprietary processor architecture�s, we are now seeing the production of specialized products derived from commercial lines. In the era of decreasing markets, the cost of entry, and of maintaining presence in this tiny market niche, are prohibitively high for many companies.
An extensive bibliography is included.
Spacecraft microprocessors are a special subset of embedded computers. Most spacecraft include 10's ro 100's of processors, doing tasks such as attitude and orbit control, power monitoring and control, telemetry formatting and command handling, data storage management, and instrument control. Without these microprocessors, the amount that we know about our neighboring planets and the intervening space would be vastly limited.
Early flight computers were custom designs, but cost and performance issues have driven the development of variants of commercial chips. Aerospace applications are usually classic embedded applications. Space applications are rather limited in number, and, until recently, almost exclusively meant NASA, ESA, or some other government agency. Flight systems electronics usually require MIL-STD-883b, Class-S, radiation-hard (total dose), SEU-tolerant parts. Specific issues of radiation tolerance are disucssed. Class-S parts are specifically for space-flight use. Because of the need for qualifying the parts for space, the state-of-the-art in spaceborne electronics usually lags that of the terrestrial commercial parts by 5 years.
Processors used in aerospace applications, as any semiconductor-based electronics, need to meet stringent selection, screening, packaging and testing requirements, and characterizations because of the unique environment. Most aerospace electronics, and the whole understanding of radiation effects, were driven by the cold war defense buildup from the 1960's through the 1980's. This era was characterized by the function-at-any-cost, melt-before-fail design philosophy. In the 1990, the byword was COTS -- use of Commercial, Off-The-Shelf products. Thus, instead of custom, proprietary processor architecture�s, we are now seeing the production of specialized products derived from commercial lines. In the era of decreasing markets, the cost of entry, and of maintaining presence in this tiny market niche, are prohibitively high for many companies.
An extensive bibliography is included.
Product Details
| BN ID: | 2940013167810 |
|---|---|
| Publisher: | PRB Publishing |
| Publication date: | 01/06/2011 |
| Sold by: | Barnes & Noble |
| Format: | eBook |
| Pages: | 49 |
| File size: | 190 KB |
About the Author
Mr. Patrick H. Stakem received a Bachelors degree in Electrical Engineering from Carnegie-Mellon University, and Masters Degrees in Physics and Compute Science from the Johns Hopkins University.
He began his career in Aerospace with Fairchild Industries on the ATS-6 (Applications Technology Satellite-6), program, a communication satellite that developed much of the technology for the TDRSS (Tracking and Data Relay Satellite System). At Fairchild, Mr. Stakem made the amazing discovery that computers were put onboard the spacecraft. He quickly made himself the expert on their support. He followed the ATS-6 Program through its operation phase, and worked on other projects at NASA�s Goddard Space Flight Center including the Hubble Space Telescope, the International Ultraviolet Explorer (IUE), the Solar Maximum Mission (SMM), some of the Landsat missions, and others. He was posted to NASA�s Jet Propulsion Laboratory for the MARS-Jupiter-Saturn (MJS-77), which later became the Voyager mission, which is still operating and returning data from outside the solar system at this writing.
Mr. Stakem is affiliated with the Computer Science Department of Loyola University in Maryland, and with the Whiting School of Engineering of the Johns Hopkins University.
He began his career in Aerospace with Fairchild Industries on the ATS-6 (Applications Technology Satellite-6), program, a communication satellite that developed much of the technology for the TDRSS (Tracking and Data Relay Satellite System). At Fairchild, Mr. Stakem made the amazing discovery that computers were put onboard the spacecraft. He quickly made himself the expert on their support. He followed the ATS-6 Program through its operation phase, and worked on other projects at NASA�s Goddard Space Flight Center including the Hubble Space Telescope, the International Ultraviolet Explorer (IUE), the Solar Maximum Mission (SMM), some of the Landsat missions, and others. He was posted to NASA�s Jet Propulsion Laboratory for the MARS-Jupiter-Saturn (MJS-77), which later became the Voyager mission, which is still operating and returning data from outside the solar system at this writing.
Mr. Stakem is affiliated with the Computer Science Department of Loyola University in Maryland, and with the Whiting School of Engineering of the Johns Hopkins University.
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