Aerostat system with extended flight envelope
An aerostat system with an extended flight envelope in which the aerostat system can safely operate is provided. The aerostat system includes an aerostat, multiple tether groups and a base station. Spatially distinct tether groups allow for improved stability and controllability over a wide range of wind conditions. Independent actuation of the tether groups allows for control of the aerostat pitch and roll angle. A rotating platform including rails to rest the aerostat allows docking without auxiliary tethers, minimizing or eliminating the ground crew required to dock traditional aerostat systems. An optional controller allows remote or autonomous operation of the aerostat system.
1. An aerostat system that allows for improved control in a variety of wind conditions, passive alignment into the wind, and autonomous docking, the system comprising:
an aerostat including a shroud;
a plurality of tether groups arranged on the shroud so that there is defined separation distance between tether attachment points in each of a longitudinal, direction and a lateral direction, each of the plurality of tether groups being independently actuated by a respective winch assembly; and
a base station located with respect to a ground surface including a rotating platform constructed to rotate about a pivot point that is located forward a mean lead-off position for the plurality of tether groups, the rotating platform being interconnected to the plurality of tether groups and including a rail assembly that selectively engages the aerostat in a docked configuration with respect to the platform.
2. The system as set forth in claim 1 , further comprising one or more forward tether lead-off points and one or more aft tether lead-off points on the base station, the one or more forward tether lead-off points being separated from the one or more aft-tether lead-off points by a lead-off-point separation distance that has a same order of magnitude as a forward and aft separation of the tether attachment points on the shroud.
3. The system as set forth in claim 2 wherein the pitch angle is a non-zero value of between approximately 5 and 10 degrees.
4. The system as set forth in claim 1 , further comprising one or more forward tether lead-off points and one or more aft tether lead-off points on the base station.
5. The system as set forth in claim 4 wherein the plurality of tether groups are arranged to define one of a three-point tether arrangement and a four-point tether arrangement.
6. The system as set forth in claim 1 , wherein the plurality of tether groups are constructed and arranged to impart a moment to both the aerostat and the rotating platform, thereby causing both components to passively align into the prevailing wind direction.
7. The system as set forth in claim 1 , wherein, in the docked configuration, the longitudinal separation of the pivot point of the rotating platform and a center of pressure of the aerostat is constructed and arranged to cause the aerostat system to passively align with a prevailing wind direction and prevents the docked aerostat from facing the wind at a high yaw angle.
8. The system of claim 1 , wherein the defined separation distance is at least equal to ten percent of a length of the aerostat.
9. The system of claim 1 , wherein the rotating platform rotates freely about the pivot point.
10. A method for tethering an aerostat that allows for improved control in a variety of wind conditions, passive alignment into the wind, and autonomous docking, the method comprising the steps of:
providing an aerostat including a shroud;
attaching a plurality of tether groups to the shroud so that there is defined separation distance between tether attachment points in each of a longitudinal, direction and a lateral direction, each of the plurality of tether groups being independently actuated by a respective winch assembly; and
attaching the plurality of tether groups to a base station located with respect to a ground surface, the base station including a rotating platform constructed to rotate about a pivot point that is located forward a mean lead-off position for the plurality of tether groups, the rotating platform including a rail assembly that selectively engages the aerostat in a docked configuration with respect to the platform.
11. The method as set forth in claim 10 , further comprising providing one or more forward tether lead-off points and one or more aft tether lead-off points on the base station, and separating the one or more forward tether lead-off points from the one or more aft-tether lead-off points by a lead-off-point separation distance that is a same order of magnitude as a forward and aft separation of the tether attachment points on the shroud.
12. The method as set forth in claim 11 wherein the pitch angle is a non-zero value of between approximately 5 and 10 degrees.
13. The method as set forth in claim 10 wherein the plurality of tether groups are arranged to define one of a three-point tether arrangement and a four-point tether arrangement.
14. The method as set forth in claim 10 , wherein the plurality of tether groups impart a moment to both the aerostat and the rotating platform, thereby causing both components to passively align into the prevailing wind direction.
15. The method as set forth in claim 10 , wherein, in the docked configuration, the longitudinal separation of the pivot point of the rotating platform and a center of pressure of the aerostat causes the aerostat system to passively align with a prevailing wind direction and prevents the docked aerostat from facing the wind at a high yaw angle.