This paper simply analysed basic conditions and velocity range in various weights of helicopter formation flight in single engine operative and performance prediction in specific weight.
The formation flight of satellites is a new area of aerospace techniques.
The paper presents a design approach based on extremum seeking for minimum power demand of formation flight of Unmanned Aerial Vehicle.
It remains to be seen how weather conditions affect the air flows that make formation flight more efficient.
It might also be hard for airlines to co-ordinate the departure times and destinations of passenger aircraft in a way that would allow them to gain from formation flight.
We also consider the effect of vortex decay over time caused by the viscidity of atmosphere in our vortex model in estimating the vortex effect experienced during the close proximity formation flight.
To solve the problem of unmanned aerial vehicle (UAV) formation flight, an approach of modeling close formation flight of UAV is presented.
This dissertation mainly investigated the design and application of autonomous formation flight control system of unmanned aerial vehicles (UAVs).
This semester's project was a study of formation flight as a means to increase economy of air transport operations.
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