Determination of a Rocket'S Attitude by a Progressive Method Using Two Reference Vectors
1966
21 pages
Report
No indication
English
Spacecraft Trajectories & Flight Mechanics , Attitude indicator , Digital computer , Solar cell , Space orientation , Angle , Angular , Attitude , Calculation , Cell , Coefficient , Computer , Digital , Error , Indicator , Magnetic , Orientation , Progression , Sensor , Signal , Solar , Spacecraft , Velocity , Translations
Engineering Index Backfile | 1961
Determination of attitude of rocket with progressive method, using only two vectors of reference
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