In an STS scenario you have all the authorizations to fly your aircraft Before the flight you must ? Observation > Evo
Set up a security perimeter on ground to keep third parties away from controlled ground area. 'controlled ground area' ground area where uas operated within which uas operator can ensure that only involved persons are present.
The mode of operation of a UAS where the unmanned aircraft constantly follows the remote pilot within a predetermined radius is called ?
2 The mode of operation of a uas where unmanned aircraft constantly follows remote pilot within a predetermined radius called Set up a security perimeter on ground to keep third parties away from controlled ground area. 'controlled ground area' ground area where uas operated within which uas operator can ensure that only involved persons are present.
The CG balance is particularly important to allow an unmanned aircraft 'fixed wing' type to have a stable equilibrium around the ?
3 The cg balance particularly important to allow an unmanned aircraft 'fixed wing' type to have a stable equilibrium around Set up a security perimeter on ground to keep third parties away from controlled ground area. 'controlled ground area' ground area where uas operated within which uas operator can ensure that only involved persons are present. 4 The movement of an unmanned aircraft fixed wing about its roll axis controlled the Set up a security perimeter on ground to keep third parties away from controlled ground area. Ailerons are horizontal surfaces usually located at trailing edge of wings they act on roll axis allowing aircraft to be banked to right or left or to keep wings levelled. 5 With regards to launcher / catapult safety areas operator must refer to Manufacturer's operating manual. Ailerons are horizontal surfaces usually located at trailing edge of wings they act on roll axis allowing aircraft to be banked to right or left or to keep wings levelled. 6 Indicate how a conventional uas multirotor controls its attitude The engines change their rotational speed (rpm) according to desired direction of flight. Ailerons are horizontal surfaces usually located at trailing edge of wings they act on roll axis allowing aircraft to be banked to right or left or to keep wings levelled. 7 In open category maximum allowable takeoff mass of an unmanned aircraft less than The engines change their rotational speed (rpm) according to desired direction of flight. It only in a3 that you can take off a uas with a mass between 4 kg less than 25 kg in open category (c3 c4 classes). 8 The remote pilot of an unmanned aircraft operating in automatic flight mode must be able to Regain manual control at any time. It only in a3 that you can take off a uas with a mass between 4 kg less than 25 kg in open category (c3 c4 classes). 9 Using this image unmanned multi rotor aircraft which will roll away from you 2 Regain manual control at any time. It only in a3 that you can take off a uas with a mass between 4 kg less than 25 kg in open category (c3 c4 classes). 10 Using this image unmanned multi rotor aircraft which will move toward you 2 Regain manual control at any time. It only in a3 that you can take off a uas with a mass between 4 kg less than 25 kg in open category (c3 c4 classes). 11 Using this image unmanned multi rotor aircraft which will roll or bank to right 2 Regain manual control at any time. It only in a3 that you can take off a uas with a mass between 4 kg less than 25 kg in open category (c3 c4 classes). 12 Using this image unmanned multi rotor aircraft which will roll or bank to left 2 Regain manual control at any time. It only in a3 that you can take off a uas with a mass between 4 kg less than 25 kg in open category (c3 c4 classes). 13 Indicate phenomenon caused the flight in ground effect Reduces induced drag. It only in a3 that you can take off a uas with a mass between 4 kg less than 25 kg in open category (c3 c4 classes). 14 Define concept of mass centering on an unmanned multirotor aircraft the centering refers to location of center of gravity cg along its Longitudinal lateral axis. It only in a3 that you can take off a uas with a mass between 4 kg less than 25 kg in open category (c3 c4 classes). 15 The lateral axis of a fixed wing drone the line that connects The tip of one wing to end of other wing tip. It only in a3 that you can take off a uas with a mass between 4 kg less than 25 kg in open category (c3 c4 classes). 16 The longitudinal axis of a fixed wing unmanned aircraft the line that connects The tail to nose of aircraft. It only in a3 that you can take off a uas with a mass between 4 kg less than 25 kg in open category (c3 c4 classes). 17 The movement of an unmanned aircraft about its longitudinal axis known as The tail to nose of aircraft. It only in a3 that you can take off a uas with a mass between 4 kg less than 25 kg in open category (c3 c4 classes). 18 Flying in ground effect will permit to an unmanned aircraft helicopter or multi rotor to hover with less power thanks to A decrease in induced drag. It only in a3 that you can take off a uas with a mass between 4 kg less than 25 kg in open category (c3 c4 classes). 19 During a straight and steady flight Lift equal to weight. It only in a3 that you can take off a uas with a mass between 4 kg less than 25 kg in open category (c3 c4 classes). 20 For a fixed wing unmanned aircraft maintaining straight and level flight 1 lift balances weight2 lift balances drag3 thrust balances drag4 thrust balances weight Lift equal to weight. It only in a3 that you can take off a uas with a mass between 4 kg less than 25 kg in open category (c3 c4 classes). Exclusive rights: Content under private and protected license, reproduction prohibited and prosecuted.
