A
hybrid aerial vehicle is optimized, for example, and not by way of limitation, to operate above 100,000 feet in altitude and provide persistent and maneuverable flight while carrying a wide array of communications and sensing payloads. The
hybrid vehicle may use the high altitude winds to
gain altitude by pitching up with the center of gravity (CG) control and using its propulsion drive to thrust into the wind to create
aerodynamic lift to rise above the
neutral buoyancy altitude. The
hybrid vehicle will
pitch down with the CG control so as to use gravity and propulsion to accelerate.
Yaw control directs the flight towards any
compass direction by rotating the gondola. This maneuvering capability permits the vehicle to
station operate persistently, even in high winds. The lighter-than-air
inflatable saucer shape is optimized for maintaining an aerodynamic cross-section to the prevailing wind from any direction in the vehicle horizontal plane. A gondola below the
saucer contains a motor, batteries, solar collector, sensors, and
yaw and CG control mechanisms.