Accession Number : AD0700660

Title :   THE DODGE ATTITUDE DETERMINATION SYSTEM.

Descriptive Note : Technical memo.,

Corporate Author : JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB

Personal Author(s) : Hickerson,R. L.

Report Date : OCT 1969

Pagination or Media Count : 91

Abstract : The report describes the DODGE satellite attitude sensors, their function, and the method of determining the satellite attitude from sensor output.

Descriptors :   (*SYNCHRONOUS SATELLITES, *SATELLITE ATTITUDE), ATTITUDE CONTROL SYSTEMS, PITCH(MOTION), ROLL, YAW, ERRORS, CALIBRATION, DETECTORS, SCIENTIFIC SATELLITES

Subject Categories : Astronautics

Distribution Statement : APPROVED FOR PUBLIC RELEASE