TY - GEN
T1 - Flight test results on navigation data based determination of air flow angles at aircraft
AU - Myschik, Stephan
AU - Holzapfel, Florian
AU - Sachs, Gottfried
PY - 2008
Y1 - 2008
N2 - A system for determining the air flow angles on-board of the aircraft and results from flight tests are presented. A computational procedure is applied for calculating the angles of attack and sideslip, using navigation data. Thus, dedicated aerodynamic sensors are not required. The system for determining the angles of attack and sideslip can be realized using miniaturized hardware components, yielding a low-cost solution. An experimental version has been built and installed in a research aircraft. Results from flight tests are presented for verification of the system.
AB - A system for determining the air flow angles on-board of the aircraft and results from flight tests are presented. A computational procedure is applied for calculating the angles of attack and sideslip, using navigation data. Thus, dedicated aerodynamic sensors are not required. The system for determining the angles of attack and sideslip can be realized using miniaturized hardware components, yielding a low-cost solution. An experimental version has been built and installed in a research aircraft. Results from flight tests are presented for verification of the system.
KW - Angles of attack and sideslip
KW - Flight test
KW - Navigation system
KW - On-board air flow angles determination
UR - http://www.scopus.com/inward/record.url?scp=79959812961&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:79959812961
SN - 9789633130117
T3 - Proceedings of the Mini Conference on Vehicle System Dynamics, Identification and Anomalies
SP - 541
EP - 548
BT - Proceedings of the 11th Mini Conference on Vehicle System Dynamics Identification and Anomalies, VSDIA 2008
T2 - 11th Mini Conference on Vehicle System Dynamics Identification and Anomalies, VSDIA 2008
Y2 - 10 November 2008 through 12 November 2008
ER -