Space Test Program - Houston 3 - Digital Imaging Star Camera (STP-H3-DISC) - 01.09.14
Science Objectives for Everyone Space Test Program - Houston 3 - Digital Imaging Star Camera (STP-H3-DISC) captures images of star fields for analysis by ground algorithms to determine the attitude of the International Space Station (ISS). The goal of this investigation is the creation of more robust and capable satellites to be controlled by ground systems for Earth-bound communications.
Science Results for Everyone Information Pending
United States Department of Defense Space Test Program, Johnson Space Center, Houston, TX, United States
Utah State University, Space Dynamics Laboratory, North Logan, UT, United States
Naval Research Laboratory, Washington, DC, United States
Sponsoring Space Agency
National Aeronautics and Space Administration (NASA)
National Laboratory - Department of Defense (NL-DoD)
ISS Expedition Duration:
March 2011 - September 2013
Previous ISS Missions
MHTEX flew as Two Phase Flow (TPF) with different heat pump and capillary loop configurations on STS-85.
CANARY is modified from a version (FLAPS) that flew as a sensor on Falcon-Sat 3 and is scheduled to fly on Falcon-Sat 5 (WISPERS).
This is the first mission for STP-H3-DISC.
- The primary goal of Space Test Program - Houston 3 - Digital Imaging Star Camera (STP-H3-DISC) is to provide a flight demonstration of a small, low power star camera capable of providing attitude (or orientation) knowledge within 0.02 degrees or better.
- The attitude information is fundamental for spacecraft control and is used to point the solar arrays toward the sun or to identify the precise geo-position of objects on the Earth.
- The development of such a control and science-enabling technology is critical for space-flight missions on small spacecraft that cannot afford the mass, power or cost of traditional star trackers, but require better pointing knowledge than current small satellite technologies can provide.
Accurate precision pointing knowledge is a critical mission requirement for many scientific and operational payloads in space. A low Size Weight And Power (SWAP) pointing sensor, such as DISC, will provide a science enabling technology on pico- and nano-satellite platforms for payloads with stringent pointing requirements.
The goals of the DISC program are to:
- 1) Develop concepts and a prototype for a low SWAP pointing system with 0.02 degrees resolution or better.
- 2) Develop processing algorithms to identify and register stellar sources. Coarse attitude solutions are used to identify the specific region of the sky of the star image. The data from the set of star images will then be used to identify and reduce the error in the star camera vector measurements.
- 3) Space-qualify the prototype unit and demonstrate performance capabilities. These goals are coupled with the primary research objective of the DISC investigation which is to successfully acquire, downlink and calculate an accurate aspect solution from the DISC image. Performance characterization of the DISC camera, including a determination of the limiting magnitude, optimal integration times, and susceptibility to scattered light are of particular interest to the research team. A series of DISC images acquired over a span of a few minutes to one orbit may also be used to investigate the on-orbit dynamics of the ELC 3 on the ISS.
The STP-H3 flight provides a proof of concept for a new low-cost, cutting-edge technology, sensing platform that strives to provide an enhanced pointing capability for nano- and pico- satellite busses. The potential benefit to the space community is the ability to provide operational data from small low cost platform versus traditional large integrated platforms such as Defense Meteorological Satellite Program (DMSP) and National Polar-orbiting Operational Environmental Satellite System (NPOESS) is significant. This technology represents a key transition from large, high cost, long-timescale programs to small, low-cost, rapid response science enabling sensing platforms.
The thermal control, attitude knowledge, and environmental sensing technologies under investigation offer a potential increase in efficiency and decrease in cost in future spacecraft design and development efforts.
One class of spacecraft that these technologies may be applied to include those incorporating earth-bound communication. The potential improvements these demonstrators will provide are in the creation of more robust and capable satellites that are controlled by ground systems.
The STP-H3 hardware complement was installed with the SSRMS and activated via ground based commands. Instrument health, status and operational data will be downlinked via standard ISS 1553 communications protocols.
DISC uses innovative technologies and instruments to record deep space images of star fields. The data will be downlinked and processed to calculate an attitude vector. The data will then be correlated with other ISS star trackers. DISC incorporates a bi-static shutter system to avoid over-exposure via direct sunlight. Operational precautions must be made to assure that DISC does not acquire images when pointing near the sun.
Concept drawing of STP-H3.
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Digital Imaging Star Camera (DISC) flight unit.
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