Abstract- An alternative solution to the velocity based self-alignment of strapdown inertial navigation system is proposed. It is well known that a simple Kalman filter based solution to the above problem fails to provide accurate azimuth alignment due to the inherent lack of observability of the model in the presence of instrument bias. Earlier researchers use external digital filters to obtain improved estimation of selected states and substitute these into the filter. The current paper demonstrates that a simple augmentation of the output vector with the inertial measurement unit signals and an extended Kalman filter would yield similar or better alignment performance compared to such ad hoc additional digital filters. The proposed metho...
GPS and Inertial Navigation Systems (INS) are increasingly used for positioning and attitude determi...
The estimation accuracy of a low-cost inertial navigation system (INS) is limited by the accuracy of...
Missile Guidance system needs accurate estimates from Inertial Navigation System (INS) for guiding t...
In this paper, a new alignment algorithm that uses simultaneously both open-loop and closedloop sch...
In this paper, an innovative inertial navigation system (INS) mechanization and the associated Kalma...
In this paper, a self-alignment method for strapdown inertial navigation systems based on the q-meth...
Navigation in autonomous vehicles involves integrating measurements from on-board inertial sensors a...
Initial alignment is always a key topic and difficult to achieve in an inertial navigation system (I...
Strapdown inertial navigation systems (INS) need an alignment process to determine the initial attit...
With the emergence of numerous low Earth orbit (LEO) satellite constellations such as Iridium-Next, ...
Abstract This paper presents an enhanced algorithm for inertial gyrocompassing using strapdown senso...
This paper presents the second part of a study aiming at the error state selection in Kalman filters...
In this paper, a coarse alignment method based on apparent gravitational motion is proposed. Due to ...
AbstractThe problem of gyrocompassing using inertial sensors, i.e., gyros and accelerometers, is add...
In GPS-aided strap-down inertial navigation system, in-motion initial alignment is crucial and can b...
GPS and Inertial Navigation Systems (INS) are increasingly used for positioning and attitude determi...
The estimation accuracy of a low-cost inertial navigation system (INS) is limited by the accuracy of...
Missile Guidance system needs accurate estimates from Inertial Navigation System (INS) for guiding t...
In this paper, a new alignment algorithm that uses simultaneously both open-loop and closedloop sch...
In this paper, an innovative inertial navigation system (INS) mechanization and the associated Kalma...
In this paper, a self-alignment method for strapdown inertial navigation systems based on the q-meth...
Navigation in autonomous vehicles involves integrating measurements from on-board inertial sensors a...
Initial alignment is always a key topic and difficult to achieve in an inertial navigation system (I...
Strapdown inertial navigation systems (INS) need an alignment process to determine the initial attit...
With the emergence of numerous low Earth orbit (LEO) satellite constellations such as Iridium-Next, ...
Abstract This paper presents an enhanced algorithm for inertial gyrocompassing using strapdown senso...
This paper presents the second part of a study aiming at the error state selection in Kalman filters...
In this paper, a coarse alignment method based on apparent gravitational motion is proposed. Due to ...
AbstractThe problem of gyrocompassing using inertial sensors, i.e., gyros and accelerometers, is add...
In GPS-aided strap-down inertial navigation system, in-motion initial alignment is crucial and can b...
GPS and Inertial Navigation Systems (INS) are increasingly used for positioning and attitude determi...
The estimation accuracy of a low-cost inertial navigation system (INS) is limited by the accuracy of...
Missile Guidance system needs accurate estimates from Inertial Navigation System (INS) for guiding t...