Add to ORKGAttitude determination systems using stellar images and star catalogs are used to obtain accurate po...
Predicting star magnitude which can be seen with naked eye or sextant through spacecraft windo
Self-stabilized vernier theodolite for determining angular orientation of line of sight between targ...
Astronomical mapping by rotating satellite to determine own angle of orientation to celestial spher
Attitude determination of spin-stabilized spacecraft using star mapping techniqu
The analysis and the FORTRAN program are presented for the determination of attitude of a spin-stabi...
The development of new instrumentation and associated data reduction programs for measuring the orie...
The goal of this research effort is to investigate the analysis, design, integration, testing, and v...
This paper provides a mathematical formulation and two solution algorithms of the problem of spacecr...
Knowing a spacecraft’s orientation is crucial for many vital functions. Attitude is often determined...
Scanning Celestial Attitude Determination System /SCADS/ for three axis attitude determination at Co...
System design analysis to establish feasibility of using electro-optical celestial scanning sensor o...
Satellite attitude determination by simulation program using Monte Carlo sampling and Kalman-Schmidt...
A mathematical formulation of the spacecraft spin axis attitude determination problem in the form of...
The Advanced Composition Explorer (ACE) spacecraft is designed to fly in a spin-stabilized attitude....
Attitude determination systems using stellar images and star catalogs are used to obtain accurate po...
Predicting star magnitude which can be seen with naked eye or sextant through spacecraft windo
Self-stabilized vernier theodolite for determining angular orientation of line of sight between targ...
Astronomical mapping by rotating satellite to determine own angle of orientation to celestial spher
Attitude determination of spin-stabilized spacecraft using star mapping techniqu
The analysis and the FORTRAN program are presented for the determination of attitude of a spin-stabi...
The development of new instrumentation and associated data reduction programs for measuring the orie...
The goal of this research effort is to investigate the analysis, design, integration, testing, and v...
This paper provides a mathematical formulation and two solution algorithms of the problem of spacecr...
Knowing a spacecraft’s orientation is crucial for many vital functions. Attitude is often determined...
Scanning Celestial Attitude Determination System /SCADS/ for three axis attitude determination at Co...
System design analysis to establish feasibility of using electro-optical celestial scanning sensor o...
Satellite attitude determination by simulation program using Monte Carlo sampling and Kalman-Schmidt...
A mathematical formulation of the spacecraft spin axis attitude determination problem in the form of...
The Advanced Composition Explorer (ACE) spacecraft is designed to fly in a spin-stabilized attitude....
Attitude determination systems using stellar images and star catalogs are used to obtain accurate po...
Predicting star magnitude which can be seen with naked eye or sextant through spacecraft windo
Self-stabilized vernier theodolite for determining angular orientation of line of sight between targ...