1-24 of 25 Books
Investigation, development, and application of optimal output feedback theory
Investigation, development, and application of optimal output feedback theory
By John R. Broussard
Computer simulation of a pilot in V/STOL aircraft control loops
Computer simulation of a pilot in V/STOL aircraft control loops
By William G. Vogt
Performance analysis of a GPS interferometric attitude determination system for a gravity gradient stabilized spacecraft
Performance analysis of a GPS interferometric attitude determination system for a gravity gradient stabilized spacecraft
By John C. Stoll
Estimating short-period dynamics using an extended Kalman filter
Estimating short-period dynamics using an extended Kalman filter
By Jeffrey E. Bauer
A real-time algorithm for integrating differential satellite and inertial navigation information during helicopter approach
A real-time algorithm for integrating differential satellite and inertial navigation information during helicopter approach
By Ty Hoang
A preliminary evaluation of an F100 engine parameter estimation process using flight data
A preliminary evaluation of an F100 engine parameter estimation process using flight data
By Trindel A. Maine
Final report for space shuttle propulsion estimation development verification
Final report for space shuttle propulsion estimation development verification
By Rogers, Robert M.
On-line range prediction system (II)
On-line range prediction system (II)
By N. Levan
Comparison of five system identification algorithms for rotorcraft higher harmonic control
Comparison of five system identification algorithms for rotorcraft higher harmonic control
By Stephen A. Jacklin
A vehicle health monitoring system for the space shuttle reaction control system during reentry
A vehicle health monitoring system for the space shuttle reaction control system during reentry
By Anthony David Rosello
A simulation study of turbofan engine deterioration estimation using Kalman filtering techniques
A simulation study of turbofan engine deterioration estimation using Kalman filtering techniques
By Heather H. Lambert
In-flight attitude estimation and control experiments with IRAS based on modern control theory
In-flight attitude estimation and control experiments with IRAS based on modern control theory
By A. P. Terpstra
An investigation of decentralized Kalman filtering as applied to integrated navigation
An investigation of decentralized Kalman filtering as applied to integrated navigation
By Joseph J. Hutton
Application of the extended Kalman filter to several formulations of orbit determination
Application of the extended Kalman filter to several formulations of orbit determination
By P. W. Chodas
Combined orbit/attitude determination for low-altitude satellites
Combined orbit/attitude determination for low-altitude satellites
By P. W. Chodas
Dynamic orbit-attitude coupling effects in the combined orbit and attitude determination for a low-altitude earth-orbiting satellite
Dynamic orbit-attitude coupling effects in the combined orbit and attitude determination for a low-altitude earth-orbiting satellite
By P. W. Chodas
Application of the extended Kalman filter to several formulations of orbit determination
Application of the extended Kalman filter to several formulations of orbit determination
By Paul Chodas
Geostationary orbital estimation using a Kalman filter
Geostationary orbital estimation using a Kalman filter
By G. B. Sincarsin
Description of data on the Nimbus 7 LIMS map archive tape
Description of data on the Nimbus 7 LIMS map archive tape
By Ellis E. Remsberg
Discrete filtering techniques applied to sequential GPS range measurements
Discrete filtering techniques applied to sequential GPS range measurements
By Frank Van Graas
Groundspeed filtering for CTAS
Groundspeed filtering for CTAS
By Gary L. Slater
Kalman filtering with inequality constraints for turbofan engine health estimation
Kalman filtering with inequality constraints for turbofan engine health estimation
By Dan Simon
Kalman filter integration of modern guidance and navigation systems
Kalman filter integration of modern guidance and navigation systems
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
A Kalman filter integrated navigation design for the IAR twin otter atmospheric research aircraft
A Kalman filter integrated navigation design for the IAR twin otter atmospheric research aircraft
By B. W. Leach