A lighter-than-air (LTA) vehicle navigation system and vehicle. The navigation system includes a first wind probing device disposed at a first probe position, wherein the first wind probing device is in communication, via a first probe communications link, with a body communication system. The navigation system also includes a second wind probing device disposed at a second probe position, wherein the second wind probing device is in communication, via a second probe communications link, with the body communication system. The navigation system also includes a wind variation detection system configured to determine wind information, including at least a wind direction, for the first wind probing device and the second wind probing device.

A lighter-than-air (LTA) vehicle navigation system and vehicle. The navigation system includes a first wind probing device disposed at a first probe position, wherein the first wind probing device is in communication, via a first probe communications link, with a body communication system. The navigation system also includes a second wind probing device disposed at a second probe position, wherein the second wind probing device is in communication, via a second probe communications link, with the body communication system. The navigation system also includes a wind variation detection system configured to determine wind information, including at least a wind direction, for the first wind probing device and the second wind probing device.

Adjustable fluidic oscillators are disclosed. A disclosed example oscillator includes a base having a cavity with a cross-sectional profile defining an oscillatory chamber between an inlet and an outlet of the oscillator, and a plunger to be received by the cavity and movable along a depth of the cavity to vary an aspect ratio of the oscillator.

Aspects of the technology include an automated system for launching lighter-than-air high altitude platforms (HAPs), in particular balloon-type HAPs. A launch system and process are employed that use cameras to observe balloon sway and other factors. A control system detects the angle and position of the balloon gas bubble in relation to the payload in real time in view of wind and other environmental factors. This, in turn, enables the control system to automatically actuate the release mechanism and launch the balloon system at a selected point in time. This mitigates issues that can occur with manual operator-controlled launches, and increases the likelihood of a successful HAP deployment in the stratosphere. Models created via machine learning enable the system to determine criteria indicating a likelihood of a successful launch. These models may be sued by the control system in order to select an appropriate point for launching the platform.

The technology provides a launch rig structure capable of filling a very large balloon envelope while the balloon is arranged vertically. The filled balloon is capable of staying aloft in the stratosphere with its payload for months or longer. The launch rig structure is configured to rotate up to 360° in response to current wind conditions. It includes an integrated lifting boom and gas handling system to fill the envelope. A payload release assembly is configured to couple with a rigid connection member of the balloon, enabling the envelope to be filled while in a vertical orientation. The payload release assembly is part of a launch cart that is positioned within the interior space of the launch rig. A gripper assembly engages with the rigid connection member. Once the envelope is filled, the gripper assembly disengages from the connection member so that the balloon floats away from the launch rig.

The technology provides a launch rig structure capable of filling a very large balloon envelope while the balloon is arranged vertically. The filled balloon is capable of staying aloft in the stratosphere with its payload for months or longer. The launch rig structure is configured to rotate up to 360° in response to current wind conditions. It includes an integrated lifting boom and gas handling system to fill the envelope. A payload release assembly is configured to couple with a rigid connection member of the balloon, enabling the envelope to be filled while in a vertical orientation. The payload release assembly is part of a launch cart that is positioned within the interior space of the launch rig. A gripper assembly engages with the rigid connection member. Once the envelope is filled, the gripper assembly disengages from the connection member so that the balloon floats away from the launch rig.

The technology relates to generating a flight map for an aircraft. For instance, this may include, running a plurality of simulations by placing a simulated aircraft within each cell of a grid representing areas of the earth and using predicted wind data. Each simulations identifies a cell in which each aircraft is located at the end of the simulation. A connection graph may be generated using any identified cells. The connection graph may be used to determine a flight map for an actual aircraft using a cost function and iterating from a destination cell to an initial cell. The flight map may be used to determine a route for the actual aircraft. In some examples, the flight map may be refined by running further simulations. The refined flight map may then be used to determine a route for the actual aircraft.

A flying object with a landing gear module serving as a floating weight that can be used simultaneously with an airship and an aerial mooring type aerostat, and more particularly, a flying object capable of simultaneously allowing a landing gear to serve as a floating weight, thereby stably simplifying a mooring process of the flying object and manufacturing the flying object at low cost.

A lighter-than-air (LTA) vehicle navigation system and vehicle. The navigation system includes a first wind probing device disposed at a first probe position, wherein the first wind probing device is in communication, via a first probe communications link, with a body communication system. The navigation system also includes a second wind probing device disposed at a second probe position, wherein the second wind probing device is in communication, via a second probe communications link, with the body communication system. The navigation system also includes a wind variation detection system configured to determine wind information, including at least a wind direction, for the first wind probing device and the second wind probing device.

A lighter-than-air (LTA) vehicle navigation system and vehicle. The navigation system includes a first wind probing device disposed at a first probe position, wherein the first wind probing device is in communication, via a first probe communications link, with a body communication system. The navigation system also includes a second wind probing device disposed at a second probe position, wherein the second wind probing device is in communication, via a second probe communications link, with the body communication system. The navigation system also includes a wind variation detection system configured to determine wind information, including at least a wind direction, for the first wind probing device and the second wind probing device.