The development of a control system to accommodate the scientific payload of the High Energy Astronomy Observatory (HEAO) is discussed. One of the critical elements of the system is the star tracker subsystem, which defines an accurate three-axis attitude reference. A digital computer program has been developed to evaluate the ability of a particular star tracker configuration to meet the requirements for attitude reference at various vehicle orientations. Used in conjuction with an adequate star catalog, the computer program provides information on availability of stars for each tracker and on the ability of the system to maintain three-axis attitude reference throughout a representative sequence of vehicle orientations
German Aerospace Center (DLR) is designing and developing a novel star tracker to be used as the pri...
The Hubble Space Telescope (HST) was launched in April 1990 to begin observing celestial space to th...
Star trackers are instruments for attitude determination and are a must for spacecrafts whereprecise...
Knowing a spacecraft’s orientation is crucial for many vital functions. Attitude is often determined...
The Advanced Composition Explorer (ACE) spacecraft is designed to fly in a spin-stabilized attitude....
A star tracker is an optical sensor that measures the relative position of stars using photocells or...
As interest in nanosatellites grows within the university community, the demand for inexpensive, spa...
Scanning Celestial Attitude Determination System /SCADS/ for three axis attitude determination at Co...
We describe an algorithm for star identification and pointing/tracking of a spaceborne electro-optic...
This report describes how guide stars are selected for the Optical Sensor Package (OSP) for the Inst...
The attitude determination and control system determines and controls the orientation of the spacecr...
A direct match technique for star identification was developed for use with the star tracker on the ...
System design analysis to establish feasibility of using electro-optical celestial scanning sensor o...
Developing an autonomous and reliable attitude determination system is one of the most crucial requi...
The goal of this research effort is to investigate the analysis, design, integration, testing, and v...
German Aerospace Center (DLR) is designing and developing a novel star tracker to be used as the pri...
The Hubble Space Telescope (HST) was launched in April 1990 to begin observing celestial space to th...
Star trackers are instruments for attitude determination and are a must for spacecrafts whereprecise...
Knowing a spacecraft’s orientation is crucial for many vital functions. Attitude is often determined...
The Advanced Composition Explorer (ACE) spacecraft is designed to fly in a spin-stabilized attitude....
A star tracker is an optical sensor that measures the relative position of stars using photocells or...
As interest in nanosatellites grows within the university community, the demand for inexpensive, spa...
Scanning Celestial Attitude Determination System /SCADS/ for three axis attitude determination at Co...
We describe an algorithm for star identification and pointing/tracking of a spaceborne electro-optic...
This report describes how guide stars are selected for the Optical Sensor Package (OSP) for the Inst...
The attitude determination and control system determines and controls the orientation of the spacecr...
A direct match technique for star identification was developed for use with the star tracker on the ...
System design analysis to establish feasibility of using electro-optical celestial scanning sensor o...
Developing an autonomous and reliable attitude determination system is one of the most crucial requi...
The goal of this research effort is to investigate the analysis, design, integration, testing, and v...
German Aerospace Center (DLR) is designing and developing a novel star tracker to be used as the pri...
The Hubble Space Telescope (HST) was launched in April 1990 to begin observing celestial space to th...
Star trackers are instruments for attitude determination and are a must for spacecrafts whereprecise...