Development of a System Identification Tool for Subscale Flight Testing
Aircraft system identification has been widely used to this day in applications like control law design, building simulators or extending flight envelopes. It can also be utilized for determining flight-mechanical characteristics in the preliminary design phase of a flight vehicle. In this thesis, t...
Main Author: | Arustei, Adrian |
---|---|
Format: | Others |
Language: | English |
Published: |
Linköpings universitet, Fluida och mekatroniska system
2019
|
Subjects: | |
Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-157292 |
Similar Items
-
On Subscale Flight Testing : Applications in Aircraft Conceptual Design
by: Sobron, Alejandro
Published: (2018) -
Conceptual Design of a Small Size Unmanned Air Vehicle : Part B: Flight Performance and Flight Mechanics
by: Bayati, Arastoo, et al.
Published: (2021) -
Simulation Model Development of a Subscale Fighter Demonstrator : Aerodynamic Database Generation and Propulsion Modeling
by: Prameswari, Carry
Published: (2017) -
Flight Mechanics of an Airship
by: Merlet, Pierre Miguel
Published: (2020) -
Developing algorithms for Flight Data Monitoring
by: Rossignol, Clémence
Published: (2020)