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3 Kaniewski P.

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Integration of INS with TACAN and altimeter

Kaniewski P.

Molecular and Quantum Acoustics

2007

Vol. 28

165-177

The paper presents a design of integrated positioning system for aircraft. The system is composed of INS, TACAN and altimeter. It employs a Complementary Extended Kalman Filter, estimating INS position, velocity and attitude errors. Chosen simulation results, comparing accuracy of INS, TACAN/ALT subsystem and integrated INS/TACAN/ALT positioning system are included.

Closed-loop INS/GNSS integrated positioning system

Kaniewski P.

Molecular and Quantum Acoustics

2007

Vol. 28

151-163

The paper describes a design of INS/GNSS positioning system for aircraft. The system is integrated according to the scheme of compensation with feed-backward INS correction and it employs a Complementary Extended Kalman Filter. It is a modified version of the system with feed-forward INS correction, also designed and published by the author [3]. The paper includes chosen results of simulations of the INS/GNSS system and a discussion of advantages of the new design.

Aircraft Positioning with INS/GNSS Integrated System

Kaniewski P.

Molecular and Quantum Acoustics

2006

Vol. 27

149-168

The paper describes methods of INS/GNSS integration and rules of designing Kalman filters. An example of INS/GPS positioning system is presented. The system employs a Complementary Linearized Kalman Filter, estimating INS position, velocity and attitude errors, as well as GPS clock bias and drift. Chosen simulation results, comparing accuracy of INS, GPS and INS/GPS are included.