Pseudomeasurement-Aided Estimation of Angle of Attack in Mini Unmanned Aerial Vehicle
Author:
Affiliation:
1. SASTRA Deemed University, Thanjavur 613 401, Tamil Nadu, India
Funder
Aeronautics Research and Development Board
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Electrical and Electronic Engineering,Computer Science Applications,Aerospace Engineering
Reference16 articles.
1. The Oxford Probe: an open access five-hole probe for aerodynamic measurements
2. Calibration of a Five-Hole Multi-Function Probe for Helicopter Air Data Sensors
3. A Monte Carlo Analysis of Sensor Fusion Algorithm for the Estimation of Aerodynamic Angles in a Mini Aerial Vehicle
4. Multistage-Fusion Algorithm for Estimation of Aerodynamic Angles in Mini Aerial Vehicle
5. Simulation and Flight Test of Autonomous Aircraft Estimation, Planning, and Control Algorithms
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