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Fault injection experiment results in space borne parallel application programs

Some, R. R.; Kim, W. S.; Khanoyan, G.; Callum, L.; Agrawal, A.; Beahan, J. J.; Shamilian, A.; Nikora, A. (2002-03-20)

The REE project has developed a fault injection suite of tools and a methodology for experimentally determining system behavior statistics in the presence of application level SEU induced transient faults.

Fault Management Architecture Assessment

Barltrop, K.; Garlan, D. (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2012., 2012-04-11)

Fault management at JPL : past, present and future

Day, John; Ingham, Michel (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2011., 2011-10-26)

Fault management design strategies

Day, John C.; Johnson, Stephen B. (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2014, 2014-05-05)

Development of dependable systems relies on the ability of the system to determine and respond to off-nominal system behavior. Specification and development of these fault management capabilities must be done in a structured ...

Fault management guiding principles

Newhouse, Marilyn E.; Friberg, Kenneth H .; Fesq, Lorraine (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2011., 2011-03-30)

Regardless of the mission type: deep space or low Earth orbit, robotic or human spaceflight, Fault Management (FM) is a critical aspect of NASA space missions. As the complexity of space missions grows, the complexity of ...

Fault management practice: a roadmap for improvement

Fesq, Lorraine M.; Oberhettinger, David (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2010, 2010-03-06)

Autonomous fault management (FM) is critical for deep space and planetary missions where the limited communication opportunities may prevent timely intervention by ground control. Evidence of pervasive architecture, design, ...

Fault mitigation schemes for future spaceflight multicore processors

Alexander, James W; Clement, Bradley J.; Gostelow, Kim P.; Lai, John Y. (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2012., 2012-06-19)

Future planetary exploration missions demand significant advances in on-board computing capabilities over current avionics architectures based on a single-core processing element. The state-of-the-art multi-core processor ...

Fault mitigation schemes for future spaceflight multicore processors

Some, Rafi; Gostelow, Kim P.; Lai, John; Reder, Leonard; Alexander, Jim; Clement, Brad (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2012., 2012-06-20)

Fault Propagation, EMI Propagation, and Fault Containment in Aerospace Systems

Perez, Reinaldo (Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2020, 2020-07-27)

The occurrence of faults in aerospace system hardware and software have consequences ranging from minor effects to catastrophic effects, and such faults can directly affect the safety of hardware and personnel. There are ...

Fault Protection Architecture for the Command and Data Subsystem on the Cassini Spacecraft

Brown, Thomas K. (1995-08)

Cassini is a NASA/JPL spacecraft that is planned to be launched in 1997 for a 10.7 year mission to

Fault protection design and testing for the Cassini spacecraft in a “mixed” thruster configuration

Bates, David; Lee, Allan; Meakin, Peter; Weitl, Raquel (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013, 2013-08-19)

NASA’s Cassini Spacecraft, launched on October 15th, 1997 and arrived at Saturn on June 30th, 2004, is the largest and most ambitious interplanetary spacecraft in history. In order to meet the challenging attitude control ...

Fault protection design and testing for the Cassini spacecraft in a “mixed” thruster configuration

Bates, David (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013, 2013-08-19)

Fault Protection Design for the Command and Data Subsystem on the Cassini Spacecraft

Brown, Thomas K.; Donaldson, James A. (1994-10-31)

The Command and Data Subsystem (CDS) on Cassini is responsible for uplink command processing, spacecraft intercommunications and control, and downlink telemetry formatting. The 10.7 year mission life, 160 minute round-trip ...

Fault Protection Design of the QuickScat And SeaWinds Instruments

Bennett, M. (1998-11-05)

The QuickScat and Sea Winds instruments are radar scatterometer instruments that will be used to measure ocean surface winds.

Fault Protection Design of the QuikScat and SeaWinds Instruments

Smith, J. F.; Bennett, M. B.; Wilkinson, W. B. (1998-10-31)

Fault protection techniques in JPL Spacecraft

Morgan, Paula S. (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2005., 2005-11-07)

While every JPL spacecraft requires some unique mission specific fault protection, there are many requirements which are common to all spacecraft configurations. These consist of protecting command and data processing & ...

Fault tolerance for matrix and signal processing applications

Katz, D. S. (2001-09-25)

Fault tolerant approaches based on evolvable hardware and using reconfigurable electronic devices

Keymeulen, D.; Stoica, A.; Zebulum, R.; Jin, Y.; Duong, V. (2000-10-23)

Fault Tolerant Architecture for Quantum Dot Cellular

Toomarian, N.; Fijany, A. (2000-10-16)

Fault Tolerant Characteristics of Artificial Neural Network Electronic Hardware

Zee, Frank (1995-05)

The fault tolerant characteristics of analog-VLSI artificial neural network (with 32 neurons and 532 synapses) chips are studied by exposing them to high energy electrons, high energy protons, and gamma ionizing radiations ...

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