1 July 1992 Space micro-guidance and control - Applications and architectures
Author Affiliations +
The features and the components of a new microscale guidance, navigation, and control (GN&C) system for future space systems are discussed. An approach is described for the utilization of new microengineering technologies for achieving major reductions in the GN&C system's mass, size, power, and costs. The micro-GN&C system and the component concepts include microactuated adaptive optics, micromachined inertial sensors, fiberoptic data nets with light-power transmission, and VLSI microcomputers. The GN&C system will be applied in microspacecraft, microlanders, microrovers, remote sensing platforms, interferometers, and deployable reflectors.
© (1992) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Edward Mettler, Fred Y. Hadaegh, "Space micro-guidance and control - Applications and architectures", Proc. SPIE 1694, Sensors and Sensor Systems for Guidance and Navigation II, (1 July 1992); doi: 10.1117/12.138116; https://doi.org/10.1117/12.138116


Integration of a fiber optic gyro AHRS into a fly...
Proceedings of SPIE (May 22 1995)
Fiber optic gyros: the vision realized
Proceedings of SPIE (August 24 2006)
The JWST fine guidance sensor
Proceedings of SPIE (October 12 2004)
A deformable secondary mirror for the VLT
Proceedings of SPIE (June 27 2006)
F-SAT attitude stabilization system
Proceedings of SPIE (September 23 1993)

Back to Top