The disclosed inventions include and apparatus and method for providing a universal Automatic Meter Reading (AMR) system configured with fly-by functionality. Such system may be configured to work in a plurality of modes including a walk-bay, drive-by, fixed network, and fly-by mode without hardware modifications. The system is configured to automatically calibrate so that the water meter transmitter operates at a minimum transmitted signal power level. Additional features include automatic hardware self-healing features where the system continues to function after certain hardware failures occur.

The disclosed inventions include and apparatus and method for providing a universal Automatic Meter Reading (AMR) system configured with fly-by functionality. Such system may be configured to work in a plurality of modes including a walk-bay, drive-by, fixed network, and fly-by mode without hardware modifications. The system is configured to automatically calibrate so that the water meter transmitter operates at a minimum transmitted signal power level. Additional features include automatic hardware self-healing features where the system continues to function after certain hardware failures occur.

A lighter than air craft having an airframe that has at least one tank in the airframe for holding compressed or liquid hydrogen or helium and at least one compartment in the airframe holding an inflatable bladder. The inflatable bladder can be inflated with hydrogen or helium gas from the first tank. There is a vent in the compartment allowing air to exit the compartment when the bladder is inflated and allowing air to enter the compartment when the bladder is deflated. Inflating and deflating the bladder partially controls buoyancy of the craft. Inflating bladders in compartments fore and aft controls pitch and trim.

A lighter than air craft having an airframe that has at least one tank in the airframe for holding compressed or liquid hydrogen or helium and at least one compartment in the airframe holding an inflatable bladder. The inflatable bladder can be inflated with hydrogen or helium gas from the first tank. There is a vent in the compartment allowing air to exit the compartment when the bladder is inflated and allowing air to enter the compartment when the bladder is deflated. Inflating and deflating the bladder partially controls buoyancy of the craft. Inflating bladders in compartments fore and aft controls pitch and trim.

An airship utilizing an innovative lift mechanism featuring dynamic and static vacuum chambers. The lift created by the vacuums created in the chambers elevates the ship into the atmosphere, thereby eliminating the need for lighter than air gases.

An airship utilizing an innovative lift mechanism featuring dynamic and static vacuum chambers. The lift created by the vacuums created in the chambers elevates the ship into the atmosphere, thereby eliminating the need for lighter than air gases.

The systems and methods provided herein are directed to a delivery system for orders from a variety of businesses located along a transport route of an aerial vehicle. Fresh food, geographically unique goods, customized goods, and other retail items are ordered by passengers while in transit over ground-based locations. Scheduled in-flight deliveries provide the ordered goods to the passengers.

In some embodiments, apparatuses and methods are provided herein useful to transport unmanned aircraft systems to delivery products. In some embodiments, gas-filled aerial transport and launch system, comprises: a transport aircraft comprising: a gas chamber; and a carrier compartment where the gas chamber induces a lifting force on the carrier compartment; at least one propulsion system; and a navigation control system that controls the direction of travel of the transport aircraft; wherein the carrier compartment comprises: an unmanned aircraft system (UAS) storage area configured to receive multiple UASs; and an UAS launching bay that enables the UAS to be launched while the transport aircraft is in flight and while the UAS is carrying a package to be delivered.

In some embodiments, apparatuses and methods are provided herein useful to transport unmanned aircraft systems to delivery products. In some embodiments, gas-filled aerial transport and launch system, comprises: a transport aircraft comprising: a gas chamber; and a carrier compartment where the gas chamber induces a lifting force on the carrier compartment; at least one propulsion system; and a navigation control system that controls the direction of travel of the transport aircraft; wherein the carrier compartment comprises: an unmanned aircraft system (UAS) storage area configured to receive multiple UASs; and an UAS launching bay that enables the UAS to be launched while the transport aircraft is in flight and while the UAS is carrying a package to be delivered.

An airship dynamic adaptive harness is provided to stabilize airships and particularly a tethered aerostat in high winds and atmospheric changes. A novel adaptive device accommodates the supply of a lift gas and simultaneously controls opposing cables in a tethered harness with a cascade control system that provides an immediate and particularly the dynamic control of roll, yaw and particularly the pitch of the aerostat in response to real time environmental flight conditions and impart stability to the airship in high winds using a stability zone geometric suspension control system and enhance the duration of in flight missions. A lifting gas replenishment system and particularly a ground based lifting gas replenishment system adds long duration deployment to the dynamic adaptability to high wind conditions for long term deployment.