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.