The Boeing Company

John L McIver

Charles Briggs Spinelli

Daniel J Gadler

Tamaira Emily Ross

Alan Eugene Bruce

Rodney B Kendrick

Ronald P Fuchs

A method and apparatus for managing a flight of an aircraft. Conditions in an environment around the aircraft are monitored during the flight of the aircraft on a route having a number of target points. In response to detecting a condition requiring a change to the route of the aircraft, current resources for the aircraft are identified. A determination is made as to whether changing the route reduces the number of target points that can be reached based on the current resources for the aircraft. In response to a determination that changing the route reduces the number of target points that can be reached, the route is changed to include a portion of the number of target points using the condition and a policy.

Management system for unmanned aerial vehicles

An inexpensive unmanned mobile sensor and data collection rolling rover ('rollver) for exploring remote, inaccessible locations, such as deep craters and canyons, includes a hollow enclosure having a flexible wall that is expandable into the shape of a sphere, an apparatus for selectably expanding the wall of the enclosure, a sensor and instrumentation payload disposed within the enclosure and coupled to an inner surface of the wall of the enclosure, and a power supply for powering the payload at its destination. The rollver is adapted to roll to a target destination at least partially in response to at least one of an initial impetus imparted to the vehicle and gravitational forces acting thereon, and due to its relatively low cost, can be simultaneously deployed and used in an area of interest in relatively large numbers.

Spherical sensor and data collection vehicles

A system including a heavier-than-air vehicle (HTA), a lighter-than-air vehicle (LTA), and a tether is disclosed. The tether is coupled between the HTA and the LTA such that the LTA supports the HTA. The system may be further configured to suit the needs of the particular application. For example, the system may be configured to be controllable from a remote location or capable of autonomous operations. The system may also be configured such that the HTA comprises a mission payload and communications equipment. In an exemplary embodiment of the invention, the LTA is configured to provide lift for the system and the HTA is configured to provide station-keeping propulsion, the advantage being reduced fuel consumption and increased mission endurance.

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Bothell, WA, United States of America

John L McIver