Applications of inertial navigation and modern control theory to the all weather landing problem
Inertial navigation and automatic landing control theory applied to instrument landing problem
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Inertial navigation and automatic landing control theory applied to instrument landing problem
Navigation and guidance simulator for identifying performance capabilities of human operator during translunar or midcourse flight
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Lunar surface navigation system accuracy in post Apollo period compared with performance requirements
Strapdown inertial navigator alignment and calibration in swaying launch vehicle on pad, using optimal recursive linear filter
Baseline navigation system for planetary missions using two way Doppler
Approach navigation accuracy for planetary atmosphere braking to orbit about Mars and Venus