San Marco satellite attitude determination based on aerodynamic drag measurements
San Marco satellite attitude determination from onboard aerodynamic drag measurements, using least squares method for three components calculation
Hunziker, R. R.↗
Engineering topics
Hunziker, R. R.
Publications and source records attributed to Hunziker, R. R..
Low-thrust station keeping guidance for a 24-hour satellite
Low thrust station keeping guidance scheme for gravity gradient stabilized 24-hour satellite, solving equations of motion for near circular equatorial orbit
Hunziker, R. R.↗
Effects of the variation of drag coefficient on the ephemeris of earth satellites
Variations after one revolution in semimajor axis, period and eccentricity computed for orbit using variable drag coefficient involving satellite and air thermal speeds
Hunziker, R. R.↗
Low thrust station keeping guidance for a 24- hour satellite.
Low thrust station keeping guidance scheme for gravity gradient stabilized 24-hour satellite, solving equations of motion for near circular equatorial orbit
Hunziker, R. R.↗