Improved Operations Capabilities to Reduce the Risk of Command-Related Error
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The Goddard Modular Smallsat Architecture (GMSA) is developed at NASA Goddard Space Flight Center (GSFC) to address future reliability along with minimizing cost and schedule challenges for NASA Cubesat and Smallsat missions.
For decades, the International Space Station (ISS) has provided a distinctive platform in low Earth orbit for experimental research. In support of this platform is a family of avionics systems that enables reliable data distribution of the many science payloads installed, and future internal and external payloads. This poster provides an update to the ISS avionics hardware system architecture, including design change successes, test bed architecture, and performance upgrades in the operation of all ISS avionics. We conclude with an outlook on future avionics system enhancements required to support additional modules and payload expansions taking place on the ISS, and how these avionics systems translate to a lunar gateway.
Description of ground support systems for the surveyor lunar-landing spacecraft
Correction of space trajectories by small midcourse maneuvers governed by impulse which is computed on the ground from radio measurements and sent by radio to the space probe
A power logic circuit, with bidirectional capability, is used to drive small loads in planned sequence. This is designed in the form of a shift register, with a reversible ring counter.
Stabilization of Lunar Mobile Laboratory VII
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Control of unmanned scientific satellites and unified tracking/command/telemetry at lunar distances
Steering system and control circuit for Lunar Surface Vehicle /LSV/ - Apollo project
Extreme value theory for estimating statistical parameters of spacecraft communication systems
Apollo Guidance and Navigation System positioning by electrically torquing gyros, discussing error sources
Star tracker error signal processor for onboard current satellite attitude control over wide range of gimbal angles
Multiple-mission telemetry system - bit-sync lock detector evaluation
Gimballed star trackers application to satellite attitude control for simplified signal processing
Data links and time reference systems in automatic navigation and flight management
Aerodynamic measurements on Apollo CM model at hypersonic flow simulating earth orbital reentry trajectory