ATTITUDE DETERMINATION OF AN ORBITING SATELLITE. PART I. GRAVITATIONAL TORQUE. PART II. DYNAMICAL EQUATIONS FOR THE ATTITUDE MATRIX. PART III. MAGNETIC TORQUE.
Abstract
This Technical Note contains a study of the effect of the earth's gravitational field on the spin-motion of an orbiting satellite. Part I discusses gravitational torque, Part II dynamical equations for the attitude matrix, and Part II magnetic torque. Two appendices and a bibliography are included. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 15, 1962
- Accession Number
- AD0609374
Entities
People
- G. Margulies
- G. S. Goodman