In order to better understand the technological difficulties involved in designing and building a sparse aperture array, the challenge of building a white light Golay-3 telescope was undertaken. The MIT Adaptive Reconnaissance Golay-3 Optical Satellite (ARGOS) project exploits wide-angle Fizeau interferometer technology with an emphasis on modularity in the optics and spacecraft subsystems. Unique design procedures encompassing the nature of coherent wavefront sensing, control and combining as well as various system engineering aspects to achieve cost effectiveness, are developed. To demonstrate a complete spacecraft in a 1-g environment, the ARGOS system is mounted on a frictionless air-bearing, and has the ability to track fast orbiting s...
oai:ojs.pkp.sfu.ca:article/75Future astronomical space missions will comprise a constellation of sev...
Sparse aperture imaging provides the opportunity to achieve high resolutions image with groups of sm...
Earth-observing satellites have fundamental size and weight design limits since they must be launche...
In order to better understand the technological difficulties involved in designing and building a sp...
In order to better understand the technological difficulties involved in designing and building a sp...
In order to better understand the technological difficulties involved in designing and building a sp...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002.Th...
Future spaceborne interferometric arrays must meet stringent optical performance and tolerance requi...
The MIT Adaptive Reconnaissance Golay-3 Optical Satellite (ARGOS) is a wide-angle Fizeau interferome...
Several future imaging missions will require large space mirrors, 10-20 m in diameter. This is a cha...
Since the first application of the telescope to astronomy in 1610, most new astronomical discoveries...
This dissertation derives and demonstrates a new approach to the design of wide-field interferometri...
Sparse-aperture telescopes are a promising technology to increase the resolution of a telescope with...
The remote sensing community continues to pursue advanced sensor designs and post processing techniq...
The Silicon Wafer Integrated Femtosatellites (SWIFT) Swarm Project presents a new paradigm-shifting ...
oai:ojs.pkp.sfu.ca:article/75Future astronomical space missions will comprise a constellation of sev...
Sparse aperture imaging provides the opportunity to achieve high resolutions image with groups of sm...
Earth-observing satellites have fundamental size and weight design limits since they must be launche...
In order to better understand the technological difficulties involved in designing and building a sp...
In order to better understand the technological difficulties involved in designing and building a sp...
In order to better understand the technological difficulties involved in designing and building a sp...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002.Th...
Future spaceborne interferometric arrays must meet stringent optical performance and tolerance requi...
The MIT Adaptive Reconnaissance Golay-3 Optical Satellite (ARGOS) is a wide-angle Fizeau interferome...
Several future imaging missions will require large space mirrors, 10-20 m in diameter. This is a cha...
Since the first application of the telescope to astronomy in 1610, most new astronomical discoveries...
This dissertation derives and demonstrates a new approach to the design of wide-field interferometri...
Sparse-aperture telescopes are a promising technology to increase the resolution of a telescope with...
The remote sensing community continues to pursue advanced sensor designs and post processing techniq...
The Silicon Wafer Integrated Femtosatellites (SWIFT) Swarm Project presents a new paradigm-shifting ...
oai:ojs.pkp.sfu.ca:article/75Future astronomical space missions will comprise a constellation of sev...
Sparse aperture imaging provides the opportunity to achieve high resolutions image with groups of sm...
Earth-observing satellites have fundamental size and weight design limits since they must be launche...