Results 131 to 140 of about 5,445 (184)
An Attitude and Heading Reference System (AHRS) based in a dual filter [PDF]
ETFA2011, 2011 Peer ...
Rodrigo Munguía, Antoni Grau
core +4 more sources
Design and validation of an attitude and heading reference system for an aerial robot prototype [PDF]
2012 American Control Conference (ACC), 2012 In this paper we consider the design and the experimental validation of an attitude and heading reference system for a miniature aerial robot prototype based on measurements obtained from a low cost off-the-shelf inertial measurement unit. Different estimation algorithms to process the raw inertial data are implemented and validated in real indoor ...
MILOSEVIC, BOJAN +4 more
core +5 more sources
Some of the next articles are maybe not open access.
Related searches:
Related searches:
Attitude and heading reference system with acceleration compensation
Aircraft Engineering and Aerospace Technology, 2012PurposeThe purpose of this paper is to employ an extended Kalman filter for implementing an AHRS (attitude and heading reference system) with acceleration compensation, thereby improving the reliability of such systems, since this removes the usual restrictive assumption that the vehicle is undergoing a non‐accelerated maneuver.Design/methodology ...
Elder M. Hemerly +3 more
openaire +3 more sources
Gimballed Attitude and Heading Reference System for Marine Vehicles
2021 IEEE 3rd Ukraine Conference on Electrical and Computer Engineering (UKRCON), 2021The paper deals with creating a gimballed attitude and heading system assigned for operation on marine vehicles. Features of the developed system are the high precision and resistance to accelerations. The kinematical scheme of the considered system is represented. The list of operating regimes is given. The mathematical models of the considered system
Olha Sushchenko
openaire +3 more sources
Gyrocompassing mode of the attitude and heading reference system
2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD), 2017A gyrocompassing mode of the attitude heading reference system was presented. Attitude heading reference system has been composed of inertial measurement unit and navigation computer. Inertial measurement unit consists of triad accelerometers, gyroscopes and a circuit of signal processing.
V. V. Avrutov +2 more
openaire +3 more sources
Attitude and Heading Reference System for Quadrotor Based on MEMS Sensors
2012 Second International Conference on Instrumentation, Measurement, Computer, Communication and Control, 2012This paper deals with designing and implementation of Attitude and Heading Reference System (AHRS) which based on data fusion of multi-sensor. And it presents an approach of designing a low cost AHRS which used Micro Electronic Mechanical System (MEMS).
Qiang Jiang +3 more
openaire +3 more sources
Inner Attitude Integration Algorithm Based on Fault Detection for Strapdown Inertial Attitude and Heading Reference System [PDF]
Chinese Journal of Aeronautics, 2010 This article proposes a new inner attitude integration algorithm to improve attitude accuracy of the strapdown inertial attitude and heading reference system(SIAHRS), which, by means of a Kalman filter, integrates the calculated attitude from the ...
Liu Jianye, Lai Jizhou
exaly +2 more sources
Development of attitude and heading reference systems
2015 International Automatic Control Conference (CACS), 2015The development of an attitude and heading reference system (AHRS) using sensor fusion is presented in this paper. The system consists of a nine degree of freedom inertial measurement unit (IMU) and a digital signal processor (DSP) module. The IMU comprises with triaxial gyroscopes, triaxial accelerometers, and triaxial magnetometers.
Yen-Hsiang Huang +2 more
openaire +1 more source
A Low Cost Attitude and Heading Reference System
2018 5th International Conference on Information Science and Control Engineering (ICISCE), 2018Real-time control should be conducted to the moving attitude during the autonomous flight of small unmanned aerial vehicle. The movement information of small unmanned aerial vehicle needed for control system is obtained through inertial measuring sensor.
Qian Zhang, Yilin Wu
openaire +1 more source
Dynamic attitude estimator for attitude and heading reference systems based on vector observations
2016 IEEE International Conference on Information and Automation (ICIA), 2016A novel attitude estimator for applications under dynamic conditions is proposed in this paper, which is based on the vector observations of gravity, geomagnetic field, and angular velocity. After a brief review of the existing solutions for attitude estimation and external acceleration rejection, we adopt the deviation of attitude, gyro bias, and ...
Xiang Li 0027, Yongjun Wang, Zhi Li
openaire +1 more source