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The Dodge Attitude Determination System.


AD700660

Publication Date 1969
Personal Author Hickerson, R. L.
Page Count 91
Abstract The report describes the DODGE satellite attitude sensors, their function, and the method of determining the satellite attitude from sensor output.
Keywords
  • Synchronous satellites
  • Satellite attitude
  • Attitude control systems
  • Pitch(Motion)
  • Roll
  • Yaw
  • Errors
  • Calibration
  • Sensors
  • Scientific satellites
  • Gravity gradient stabilization
  • DODGE(DOD Gravity Experiment)
  • DOD gravity experiment
  • DODGE satellite
  • Spaceborne photography
NTIS Subject Category
  • 84A - Astronautics
Corporate Authors Johns Hopkins Univ Silver Spring MD Applied Physics Lab
Document Type Technical Report
Title Note Technical memo.
NTIS Issue Number 197007
Contract Number
  • NOW-62-0604
The Dodge Attitude Determination System.
The Dodge Attitude Determination System.
AD700660

  • Synchronous satellites
  • Satellite attitude
  • Attitude control systems
  • Pitch(Motion)
  • Roll
  • Yaw
  • Errors
  • Calibration
  • Sensors
  • Scientific satellites
  • Gravity gradient stabilization
  • DODGE(DOD Gravity Experiment)
  • DOD gravity experiment
  • DODGE satellite
  • Spaceborne photography
  • 84A - Astronautics
  • NOW-62-0604
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