ebook img

NASA Technical Reports Server (NTRS) 20110016550: Micro Sun Sensor for Spacecraft PDF

0.12 MB·English
Save to my drive
Quick download
Download
Most books are stored in the elastic cloud where traffic is expensive. For this reason, we have a limit on daily download.

Preview NASA Technical Reports Server (NTRS) 20110016550: Micro Sun Sensor for Spacecraft

Electronics/Computers Micro Sun Sensor for Spacecraft NASA’s Jet Propulsion Laboratory, Pasadena, California A report describes the development mask containing a rectangular array of the pinhole Sun images on the APS. of a compact micro Sun sensor for use microscopic pinholes, machined utiliz- The Sun angle, relative to a coordinate as a part of the attitude determination ing the microectromechanical systems system fixed to the sensor unit, is then subsystem aboard future miniature (MEMS), is mounted in front of an ac- computed from the positions of the spacecraft and planetary robotic vehi- tive-pixel sensor (APS) image detector. centroids. cles. The prototype unit has a mass of The APS consists of a 512×512-pixel This work was done by Sohrab Mobasser, only 9 g, a volume of only 4.2 cm3, a array, on-chip 10-bit analog to digital Carl Liebe, Youngsam Bae, Jeffrey power consumption of only 30 mW, and converter (ADC), on-chip bias genera- Schroeder, and Chris Wrigley of Caltech for a 120° field of view. The unit has tion, and on-chip timing control for NASA’s Jet Propulsion Laboratory. demonstrated an accuracy of 1 arc- self-sequencing and easy programma- Further information is contained in a TSP minute. The unit consists of a multiple- bility. The digitized output of the APS is (see page 1) pinhole camera: A micromachined processed to compute the centroids of NPO-30867 Passive IFF: Autonomous Nonintrusive Rapid Identification of Friendly Assets Targeting decisions could be made with speed needed in urgent situations. NASA’s Jet Propulsion Laboratory, Pasadena, California A proposed optoelectronic instru- capability of the optical correlator An optical correlator that has been ment would identify targets rapidly, with- would be exploited to obtain rapid under development for several years out need to radiate an interrogating sig- identification of a set of probable tar- and that has been demonstrated to be nal, apply identifying marks to the gets within a scene of interest and to de- capable of tracking a cruise missile targets, or equip the targets with fine regions within the scene for the might be considered a prototype of the transponders. The instrument was con- neural processor to analyze. The neural optical correlator in the proposed IFF ceived as an identification, friend or foe processor would then concentrate on instrument. This optical correlator fea- (IFF) system in a battlefield setting, each region selected by the optical cor- tures a 512-by-512-pixel input image where it would be part of a targeting sys- relator in an effort to identify the tar- frame and operates at an input frame tem for weapons, by providing rapid get. Depending on whether or not a tar- rate of 60 Hz. It includes a spatial light identification for aimed weapons to help get was recognized by comparison of its modulator (SLM) for video-to-optical in deciding whether and when to trigger image data with data in an internal image conversion, a pair of precise them. The instrument could also be database on which the neural processor lenses to effect Fourier transforms, a fil- adapted to law-enforcement and indus- was trained, the processor would gener- ter SLM for digital-to-optical correla- trial applications in which it is necessary ate an identifying signal (typically, tion-filter data conversion, and a to rapidly identify objects in view. “friend” or “foe”). The time taken for charge-coupled device (CCD) for detec- The instrument would comprise this identification process would be less tion of correlation peaks. In operation, mainly an optical correlator and a than the time needed by a human or ro- the input scene grabbed by a video sen- neural processor (see figure). The in- botic gunner to acquire a view of, and sor is streamed into the input SLM. Pre- herent parallel-processing speed and aim at, a target. computed correlation-filter data files representative of known targets are then Optical Correlator Neural Processor downloaded and sequenced into the fil- ter SLM at a rate of 1,000 Hz. When (cid:127)Wide-Area search there occurs a match between the input (cid:127)Noise/Clutter (cid:127)Recognition, target data and one of the known-target Preprocessing Classification, and Imaged Optics and (cid:127)Detection of Target of Identification of Instrument data files, the CCD detects a correlation Scene Sensor Suite Interest Targets Over Regions Output peak at the location of the target. Dis- Containing Targets of (cid:127)Parallel Processing tortion-invariant correlation filters from Interest with Inherent Shift a bank of such filters are then se- Variance quenced through the optical correlator for each input frame. The net result is An Optical Correlator and a Neural Processor, each performing a different portion of the overall tar- the rapid preliminary recognition of get-identification task, would generate a signal indicative of the identity of a target (e.g., “friend” or one or a few targets. “foe”) in a fraction of a second. NASA Tech Briefs, January 2004 9

See more

The list of books you might like

Most books are stored in the elastic cloud where traffic is expensive. For this reason, we have a limit on daily download.