C. E. Cohen

发表

High Integrity GPS-Based Precision Landing Using In Beacon Pseudolites

B. Pervan, D. Lawrence, J. Powell, 1995 .

Architectures for Joint GPS/LEO Satellite Carrier Phase Receivers Designed for Rapid Robust Resolution of Carrier Cycle Ambiguities on Mobile Platforms

M. Rabinowitz, B. W. Parksinson, K. Gromov, 2000 .

Real-Time Flight Test Evaluation of the GPS Marker Beacon Concept for Category III Kinematic GPS Precision Landing

Bradford W. Parkinson, J. David Powell, Boris Pervan, 1993 .

Flight Test Results of Autocoupled Approaches Using GPS and Integrity Beacons

Andrew K. Barrows, Bradford W. Parkinson, J. David Powell, 1994 .

Augmenting Kinematic GPS With a Pulsed Pseudolite to Improve Navigation Performance

Per Enge, Bradford W. Parkinson, J. David Powell, 1996 .

Theory and Design of Pseudolites

H. S. Cobb, B. Parkinson, C. E. Cohen, 1994 .

Estimation of gyroscope polhode motion using trapped magnetic flux

G. Keiser, B. Parkinson, C. E. Cohen, 1992 .

Analysis of spacecraft attitude measurements using onboard GPS

Bradford W. Parkinson, E. Glenn Lightsey, Clark E. Cohen, 1994 .