A vertical takeoff and landing aircraft, using for vertical lift and lateral thrust a redundant plurality of essentially similar electrically-powered and electronically-controlled thrust units mounted in a mechanically static or fixed fashion relative to one another in a substantially horizontal plane. The thrust units are situated in this planar array in aerodynamically approximate pairs, such that a complete failure of a single thrust unit would not substantially compromise the ability of the aircraft to maintain flight.

 
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< Method and apparatus for assigning weighting coefficients for performing attitude calculations with a star sensor

> Small unmanned airborne vehicle airframe

> PAV regions for encapsidation and E1 transcriptional control

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