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Developing an Attitude and Heading Reference System based on Advanced MEMS Gyros

AIAA Infotech @ Aerospace, 2015
Attitude measurement performance onboard aeronautical transport platforms is a key issue to enanche mission capabilities of current systems. Indeed, the standard attitude measurement accuracy FAA requirements, i.e. 1° rms for pitch and roll and 3° rms for heading, are intended for typical mission profiles that where adopted in the past.
Accardo, Domenico   +3 more
openaire   +2 more sources

Secure Estimation for Attitude and Heading Reference Systems Under Sparse Attacks

IEEE Sensors Journal, 2019
This paper focuses on the problem of secure attitude estimation for autonomous vehicles. Based on the established AHRS measuring model and the attack model, we have decomposed the optimal Kalman estimate into a linear combination of local state estimates.
Rui Jiang   +3 more
openaire   +2 more sources

Invariant observer design of attitude and heading reference system

Control Theory and Technology, 2019
An attitude and heading reference system (AHRS) is a nonlinear state estimator unit for computing orientation in 3D space. This paper designs an AHRS using three approaches: an invariant observer, an invariant extended Kalman filter (IEKF), and a conventional extended Kalman filter (EKF).
openaire   +1 more source

GNSS-Based Dual-Antenna Heading Augmentation for Attitude and Heading Reference Systems

ION GNSS+, The International Technical Meeting of the Satellite Division of The Institute of Navigation, 2016
Many current high-end avionics installations utilize redundant Inertial Navigation Systems (INS) with very high quality Inertial Measurement Units (IMUs) in order to maintain high accuracy heading with integrity. Attitude and Heading Reference Systems (AHRSs) that provide less accurate heading are frequently used on smaller business and regional ...
Bernard Schnaufer   +3 more
openaire   +1 more source

Survey on Attitude and Heading Reference Systems for Remotely Piloted Aircraft Systems

2014 International Conference on Unmanned Aircraft Systems (ICUAS), 2014
Attitude estimation is a critical task for the safe navigation of RPAS (Remotely Piloted Aircraft System). When no 3D positioning information is available, e.g. due to GNSS (Global Navigation Satellite System) blockage, the autopilot must use data from the rest of the onboard navigation sensors to fly the RPAS in a stable manner and reduce potential ...
Miguel Cordero   +4 more
openaire   +1 more source

Low-cost Attitude and Heading Reference System: Filter design and experimental evaluation

2010 IEEE International Conference on Robotics and Automation, 2010
This paper presents the design and performance evaluation of a low-cost Attitude and Heading Reference System (AHRS) for autonomous vehicles. A single sensor pack, an Inertial Measurement Unit (IMU), provides all the data required to feed the attitude filter.
Pedro Tiago Martins Batista   +3 more
openaire   +1 more source

Software algorithms in air data attitude heading reference systems

Aircraft Engineering and Aerospace Technology, 2003
An introduction to air data attitude heading reference systems (ADAHRS) is presented along with the developments and discussion of software algorithms used in such systems. Both Kalman filtering and fuzzy logic adaptive signal processing are presented and discussed.
Michael E. Greene, Victor Trent
openaire   +1 more source

Optimization of Control Parameter for Filter Algorithms for Attitude and Heading Reference Systems

2018 IEEE Congress on Evolutionary Computation (CEC), 2018
An Attitude and Heading Reference System (AHRS) provides orientation information of an object such as an Unmanned Air Vehicle by fusing sensor data from a magnetic and inertial measurement unit (MIMU). A MIMU consists of three components, which are a gyroscope, an accelerometer and a magnetometer.
openaire   +1 more source

Design of Attitude and Heading Reference System Based on DSP and STM32

2019 Chinese Control And Decision Conference (CCDC), 2019
This paper based on the DSP and STM32 single-chip microcomputer, adopting multi-sensor data fusion to carry out the Kalman filter as the aerial pose solution unit, the core part of a posture reference system is designed in this paper. A three-axis multifunctional turntable SGT320E is selected to analyze and verify the data in static and dynamic ...
Luo Dan, Gao Guowei
openaire   +1 more source

Design of attitude and heading reference system based on MEMS sensor

2012 24th Chinese Control and Decision Conference (CCDC), 2012
This paper presents a design scheme of attitude and heading reference system (AHRS) which consists of low cost MEMS sensors, magnetometers and related data fusion algorithms, based on the chosen sensors and algorithms, the simulation is performed to assess the structure of algorithms, computational burden and convergence from the engineering view of ...
Zhiping Liu, null Lili Wu
openaire   +1 more source

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