Longitudinal flight control with a variable span morphing wing
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![Figure 2.3 Forces and angles concerning the longitudinal flight plane analysis [3][12]](https://thumb-eu.123doks.com/thumbv2/123dok_br/18691062.915182/50.892.122.731.591.930/figure-forces-angles-concerning-longitudinal-flight-plane-analysis.webp)
![Figure 2.5 Pressure distribution along the tail’s horizontal empennage and elevator and its change due to elevator defection [3][12]](https://thumb-eu.123doks.com/thumbv2/123dok_br/18691062.915182/52.892.185.673.674.899/figure-pressure-distribution-horizontal-empennage-elevator-elevator-defection.webp)
![Figure 3.1 Olharapo light UAV prototype featuring its standard wing configuration [48]](https://thumb-eu.123doks.com/thumbv2/123dok_br/18691062.915182/73.892.182.748.697.1124/figure-olharapo-light-uav-prototype-featuring-standard-configuration.webp)
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