WO2021072065A1
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Hybrid power systems for different modes of flight
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Electric vertical take-off and landing vehicle with wind turbine
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Charging station for self-balancing multicopter
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Site local servers for vehicle management
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Spring-loaded flaps for air cooling in a wet environment
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Distance sensor test system
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Recovery system using vehicle state information
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Flexible battery system for a vehicle
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Fixed wing aircraft with trailing rotors and T-tail
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Altitude estimation using differential pressure sensors in ground effect
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Modular personal transportation system
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Charge related processing for a personal transportation system with removable battery
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Two vehicle transportation system
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Parachute architecture for low-altitude VTOL aircraft
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Battery shifting for center of gravity control
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Propeller with passive variable pitch and rotatable base
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Multicopter with wide span rotor configuration and protective fuselage
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Variable sensitivity input device for vehicle
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Preferred break points and paths in airframes for ballistic parachute systems
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Health based actuator allocation
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