Inertial navigation equations are developed which use area navigation (RNAV) waypoints and runway references as coodinate centers. The formulation is designed for aided inertial navigation systems and gives a high numerical accuracy through all phases of flight. A new formulation of the error equations for inertial navigation systems is also presented. This new formulation reduces numerical calculations in the use of Kalman filters for aided inertial navigation systems
Main issues of integrated inertial navigation were presented including inertial navigation equations...
The objective of this work is to develop an alternative INS aiding source other than the GPS, while ...
Self alignment techniques for strapdown inertial navigation systems for commercial aircraf
A description of work whose broad objective is to attain improved aircraft navigation performance th...
An inertial navigation system utilizing a servo-controlled two degree of freedom pendulum to obtain ...
An evaluation is presented of the approach and landing performance of a Kalman filter aided inertial...
NAVSIM II, a computer program for analytical simulation of aided-inertial navigation for aircraft, i...
Navigation is defined as the process of estimating the six degrees of freedom. We have seen an incre...
The aiding of an INS using measurements over time of the line of sight of ground features as they co...
Four candidate navigation systems for the space shuttle orbiter approach and landing phase are evalu...
Improved automatic landing systems for aircraft by applying control theory and inertial navigation d...
Digital computer program for performance analysis of all inertial guidance system along reference tr...
Derivation of three-dimensional three-degree-of- freedom reentry equations of motion in terrestrial ...
The problems in navigation and guidance encountered by aircraft in the initial transition period in ...
Error analysis of strapdown and local level inertial navigation systems which compute in geographic ...
Main issues of integrated inertial navigation were presented including inertial navigation equations...
The objective of this work is to develop an alternative INS aiding source other than the GPS, while ...
Self alignment techniques for strapdown inertial navigation systems for commercial aircraf
A description of work whose broad objective is to attain improved aircraft navigation performance th...
An inertial navigation system utilizing a servo-controlled two degree of freedom pendulum to obtain ...
An evaluation is presented of the approach and landing performance of a Kalman filter aided inertial...
NAVSIM II, a computer program for analytical simulation of aided-inertial navigation for aircraft, i...
Navigation is defined as the process of estimating the six degrees of freedom. We have seen an incre...
The aiding of an INS using measurements over time of the line of sight of ground features as they co...
Four candidate navigation systems for the space shuttle orbiter approach and landing phase are evalu...
Improved automatic landing systems for aircraft by applying control theory and inertial navigation d...
Digital computer program for performance analysis of all inertial guidance system along reference tr...
Derivation of three-dimensional three-degree-of- freedom reentry equations of motion in terrestrial ...
The problems in navigation and guidance encountered by aircraft in the initial transition period in ...
Error analysis of strapdown and local level inertial navigation systems which compute in geographic ...
Main issues of integrated inertial navigation were presented including inertial navigation equations...
The objective of this work is to develop an alternative INS aiding source other than the GPS, while ...
Self alignment techniques for strapdown inertial navigation systems for commercial aircraf