MOMENTUM CONTROL OF THE OAO SPACECRAFT UTILIZING THE EARTH'S MAGNETIC FIELD
Oao spacecraft momentum regulated by torque created by the interaction of current carrying coils with the earth magnetic field
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Oao spacecraft momentum regulated by torque created by the interaction of current carrying coils with the earth magnetic field
Onboard digital computer and strap-down inertial reference unit for attitude control of advanced OAO
Environmental testing, spacecraft configuration, data retrieval and flight simulation in OAO EXPERIMENTS
Calibration of star tracker bias errors on OAO
Reduction of OAO spacecraft data handling equipment telemetry data
Stability criteria for OAO coarse pointing mode
OAO-C spacecraft optical and electronics Princeton Experiment Package including telescope, spectrometer, guidance sensor and power supply
Fine guidance sensor for OAO, detailing sample and hold circuit design to solve error problems from electro-optical elements
Explicit guidance equations for Atlas/Centaur launch vehicle provides steering and engine cutoff commands for OAO, ATS and Mariner interplanetary missions
OAO satellite attitude control maintained by star trackers and momentum wheels, using Liapunov technique
In-orbit star tracker misalignment estimation on OAO
Design, testing and final characteristics of OAO gimballed star tracker
Spaceborne stored program computer design for OAO-C, noting auxiliary command storage, spacecraft monitoring and malfunction reporting, etc
Atlas Centaur 16 flight performance in injecting OAO-2 into nearly circular earth orbit
Design requirements for high-voltage circuitry in star tracker of OAO
Structures and subsystems of space telescopes for OAO program
Primary position reference system for stabilization and control of OAO spacecraft