Unified error analysis of terrestrial inertial navigation systems
Unified error analysis application to altimeter- aided terrestrial inertial navigation systems
Britting, K. R.↗
Engineering topics
Britting, K. R.
Publications and source records attributed to Britting, K. R..
Study of the concept of inertially aided barometric altimetry system for supersonic aircraft
Study of concept of inertially aided barometric altimetry system to meet vertical separation requirements of 1000 and 2000 feet for Mach 3.5 aircraft in altitude hold at 80,000 feet
Britting, K. R.↗
Inertial navigation systems analysis.
This volume offers the avionic systems engineer a fundamental exposition of the mechanization and error analysis of inertial navigation systems. While the material is applicable to spacecraft and undersea navigation, emphasis is placed upon terrestrial applications on or slightly above the earth's surface. As a result, practical considerations are geared toward those aircraft navigation systems of particular current interest. Extensive use is made of perturbation techniques to develop linearized system equations, whose solutions closely approximate those obtained by nonlinear differential equations. A unified error analysis technique is developed that is applicable to virtually all system configurations. The technique provides a greatly simplified method for comparing the performance of competing system configurations.
Britting, K. R.↗
A study of problems in aircraft navigation and control Final report
Investigating performance of various types of pure inertial and hybrid navigation systems
Britting, K. R.↗
Self-alignment techniques for strapdown inertial navigation systems with aircraft application
Commercial aircraft strapdown inertial navigation systems, examining initial self alignment techniques
Britting, K. R.↗
Error analysis of strapdown and local level inertial systems which compute in geographic coordinates
Error analysis of strapdown and local level inertial navigation systems which compute in geographic coordinates
Britting, K. R.↗
Strapdown navigation equations for geographic and tangent coordinate frames
Navigation equations for geographic and tangent coordinate frames for radar strapdown inertial navigation
Britting, K. R.↗
State transition matrix for inertial navigation systems
Error equation for inertial navigation systems formulated and solved in state space notation
Britting, K. R.↗
Self alignment techniques for strapdown inertial navigation systems with aircraft application
Self alignment techniques for strapdown inertial navigation systems for commercial aircraft
Britting, K. R.↗
Analysis of space stabilized inertial navigation systems
Analysis of space stabilized inertial navigation systems
Britting, K. R.↗