Loon LLC

Aerostar International, Inc.

Google Inc.

Softbank Corporation

Sameera Sylvia Ponda

Salvatore J Candido

Jacques L Gagne

Matthew Aaron Knoll

Michael Eglington

Jacob Buswell Roberts

Daniel Alex Luebke

Jonathan Nutzmann

Ewout Van Bekkum

Aaron Fan

Richard Wayne Devaul

Kevin Roach

Nlkhil Singh Kohli

Aspects of the technology relate to propulsion systems for high altitude, long duration balloons, such as balloons that operate in the stratosphere for weeks, months or longer. A propeller assembly is used to provide lateral directional adjustments, which allows the balloon to spend more time over a desired region, reduce the return time to the desired region, reduce fleet overprovisioning, and increases the safety case by additional controls and avoidance abilities. A control assembly manages operation of the propeller assembly, including setting the pointing direction, speed of rotation and determining when to turn on the propeller and for how long. The propulsion system including the control and propeller assemblies is rotatable around a connection member of the balloon. Such rotation is independently adjustable from any rotation of the balloon's payload. The propeller blades may be made of plastic, which reduces weight and cost while providing sufficient speed at stratospheric altitudes.

Lateral propulsion systems and architectures for high altitude balloons

Methods and systems for controlling a group of aerial vehicles to meet a connectivity service objective are provided. A method may include causing aerial vehicles in the group to arrive at a target service area during a given arrival time window associated with the connectivity service objective, which may indicate a desired probability of service coverage of the target service area. The method further includes calculating a probability of service coverage of the target service area for the vehicles for a time period after the vehicles are expected to arrive at the target service area, determining whether the probability of service coverage meets a threshold, and causing the vehicles to operate according to a station seeking flight policy during the time period.

Delivering connectivity to a service area by aerial vehicles using probabilistic methods

A system for controlling an aerial vehicle includes an aerial vehicle, a ballast coupled to the aerial vehicle, a server including a processor and a memory, and a wireless communication link that communicatively couples the aerial vehicle and the server. the memory stores instructions that, when executed by the processor, cause the server to receive weather data, determine, based on the weather data, that the aerial vehicle is experiencing, or is expected to experience, weather that satisfies a predetermined criterion, and cause the aerial vehicle to decouple at least a portion of the ballast based on a result of the determination.

Aerial vehicle control using ballast

Disclosed are systems, devices, and methods for controlling an aerial vehicle. An exemplary method may include receiving data indicating a location and an altitude of the aerial vehicle, receiving prevailing wind pattern data regarding winds at the location and the altitude of the aerial vehicle, selecting a heading for the aerial vehicle based on the prevailing wind pattern data, and causing the aerial vehicle to adjust the altitude of the aerial vehicle based on the selected heading.

Systems and methods for controlling aerial vehicles

A system for estimating aerial vehicle status includes an aerial vehicle, a computing device, and a wireless communication link that communicatively couples the aerial vehicle and the computing device. The aerial vehicle includes a sensor that outputs telemetry data. The computing device includes a processor and a memory. The memory stores instructions that, when executed by the processor, cause the computing device to retrieve the telemetry data from the sensor via the wireless communication link, execute an estimation algorithm based at least in part on the telemetry data, and determine a state of the aerial vehicle based on a result of the estimation algorithm.

Estimation of aerial vehicle state

Disclosed are systems, devices, and methods for controlling an aerial vehicle. An exemplary method may include receiving data indicating a location and an altitude of the aerial vehicle, receiving data indicating a destination of the aerial vehicle, determining a vector from the location of the aerial vehicle to the destination of the aerial vehicle, receiving prevailing wind pattern data regarding winds at the location and altitude of the aerial vehicle, planning a path for the aerial vehicle to move along the vector based on the prevailing wind pattern data, and causing the aerial vehicle to adjust the altitude of the aerial vehicle based on the prevailing wind pattern data and the planned path.

Disclosed are systems, devices, and methods for controlling an aerial vehicle. An exemplary method may include receiving data indicating a location and an altitude of the aerial vehicle, receiving data indicating a destination of the aerial vehicle, receiving prevailing wind pattern data regarding winds at the location and altitude of the aerial vehicle, determining that the aerial vehicle is within a predetermined distance of the destination, determining a speed at which the aerial vehicle is moving, and causing the aerial vehicle to adjust the altitude of the aerial vehicle based on the prevailing wind pattern data and the determined speed.

An example system includes a battery, a controllable heating element arranged to heat the battery, a load coupled to the battery, and a controller configured to: determine a current temperature of the battery; determine a SOC of the battery; based on the current temperature of the battery, select a setpoint profile from a plurality of setpoint profiles for the battery, where each of the plurality of setpoint profiles has a temperature association, and where each of the plurality of profiles comprises one or more temperature setpoints; based on a comparison of the current SOC and a SOC of the selected setpoint profile, determine a current temperature setpoint from the one or more temperature setpoints of the selected setpoint profile; and in response to determining the current temperature setpoint of the battery, cause the current temperature of the battery to adjust according to the current temperature setpoint of the battery.

Dynamic battery pack thermal management

A balloon having a balloon envelope that is fillable with a first lifting gas, a top plate arranged at a top of the balloon envelope, an outlet port that provides a passageway from an inside of the balloon envelope to the atmosphere, an inner bladder positioned within the balloon envelope and positioned at the top of the balloon envelope and coupled to the top plate, wherein the inner bladder is fillable with a second lifting gas, wherein the outlet port is configured to vent the first lifting gas to the atmosphere while keeping the second lifting gas in the inner bladder.

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Mountain View, CA, United States of America

Sameera Sylvia Ponda