• No results found

Fault-tolerant flight control for a fixed-wing unmanned aerial vehicle with partial horizontal and vertical stabiliser losses

N/A
N/A
Protected

Academic year: 2021

Share "Fault-tolerant flight control for a fixed-wing unmanned aerial vehicle with partial horizontal and vertical stabiliser losses"

Copied!
162
0
0

Loading.... (view fulltext now)

Full text

Loading

Figure

Figure 1.1: Trainer 60 RC aircraft
Figure 1.2: Hardware overview
Figure 2.1: Inertial reference frame
Figure 2.8: Standard aircraft model
+7

References

Related documents

More broadly, most economic and financial crimes in Russia and other former Soviet Union economies are associated with organized crime groups [62]... Some examples of

Central to the success of IOOS, and other regional, national, and international ocean and coastal observing systems, is the presence of a Data Management and Communications

A Lawyers Collective survey of police officers indicates that police in Delhi and Rajasthan believe that, in situations of domestic violence, the personal safety of a woman is

Watary-UM, Museum of Cantemporary Art, Tokyo, Japan Museo Nacional de Bellas Artes, La Habana, Cuba Galleria Civica, Modena, Italy. Museum Ludwig, Köln, Germany Museum of

State Agencies participating in the 13/14 RMWCP Premium Reduction Program must have completed an application (SFN 53425) within 60 days after the beginning of the RMWCP premium

Pursuant to Federal Rules of Appellate Procedure 15(d) and 27 and Rule 27.1 of the Local Rules and Internal Operating Procedures of the Court of Appeals for the Second

Under these conditions surface free energy always favors solid wrapping up a droplet providing the Young’s law contact angle is greater than zero. All smooth (r=1) solids with

A survey of breast characteristics (compressed breast thickness, peak breast density) and AGD values was carried out on a database describing the acquisition conditions