Methods and systems for transitioning an aerial vehicle between hover flight and crosswind flight

1. A method comprising:

operating an aerial vehicle in a hover-flight orientation, wherein the aerial vehicle is connected to a tether that defines a tether sphere having a radius based on a length of the tether, wherein the tether is connected to a ground station;

while the aerial vehicle is in the hover-flight orientation, positioning the aerial vehicle at a first location that is on the tether sphere, wherein the first location is downwind of the ground station;

transitioning the aerial vehicle from the hover-flight orientation to a forward-flight orientation, such that the aerial vehicle moves from the tether sphere, wherein the aerial vehicle has attached flow, and wherein a tension of the tether is reduced; and

operating the aerial vehicle in the forward-flight orientation to ascend at an angle of ascent to a second location that is on the tether sphere, wherein the second location is downwind of the ground station.

2. The method of claim 1 , wherein operating the aerial vehicle in the forward-flight orientation to ascend at the angle of ascent to the second location comprises selecting a maximum angle of ascent, such that the aerial vehicle has attached flow during the ascent.

3. The method of claim 2 , wherein operating the aerial vehicle in the forward-flight orientation to ascend at the angle of ascent to the second location comprises adjusting a pitch angle of the aerial vehicle based on the maximum angle of ascent.

4. The method of claim 1 , wherein a bottom of the tether remains above a predetermined altitude.

5. The method of claim 1 , further comprising transitioning the aerial vehicle from the forward-flight orientation to a crosswind-flight orientation.

6. A system comprising:

a tether connected to a ground station, wherein the tether defines a tether sphere having a radius based on a length of the tether;

an aerial vehicle connected to the tether; and

a control system programmed to:

operate the aerial vehicle in a hover-flight orientation;

while the aerial vehicle is in the hover-flight orientation, position the aerial vehicle at a first location that is on the tether sphere, wherein the first location is downwind of the ground station;

transition the aerial vehicle from the hover-flight orientation to a forward-flight orientation, such that the aerial vehicle moves from the tether sphere, wherein the aerial vehicle has attached flow, and wherein a tension of the tether is reduced; and

operate the aerial vehicle in the forward-flight orientation to ascend at an angle of ascent to a second location that is on the tether sphere, wherein the second location is downwind of the ground station.

7. The system of claim 6 , wherein the control system is further programmed to select a maximum angle of ascent, such that the aerial vehicle has attached flow during the ascent.

8. The system of claim 7 , wherein the control system is further programmed to adjust a pitch angle of the aerial vehicle based on the maximum angle of ascent.

9. The system of claim 6 , wherein the control system is further programmed to operate the aerial vehicle in the hover-flight orientation, such that a bottom of the tether remains above a first predetermined altitude,

wherein the control system is further programmed to, while the aerial vehicle is in the hover-flight orientation, position the aerial vehicle at the first location, such that the bottom of the tether remains above a second predetermined altitude,

wherein the control system is further programmed to transition the aerial vehicle from the hover-flight orientation to the forward-flight orientation, such that the bottom of the tether remains above the second predetermined altitude, and

wherein the control system is further programmed to operate the aerial vehicle in the forward-flight orientation to ascend at the angle of ascent to the second location, such that the bottom of the tether remains above the second predetermined altitude.

10. The system of claim 6 , wherein the control system is further programmed to transition the aerial vehicle from the forward-flight orientation to a crosswind-flight orientation.

11. A method comprising:

operating an aerial vehicle in a hover-flight orientation, wherein the aerial vehicle is connected to a tether that defines a tether sphere having a radius based on a length of the tether, wherein the tether is connected to a ground station;

while the aerial vehicle is in the hover-flight orientation, positioning the aerial vehicle at a first location that is on the tether sphere, wherein the first location is downwind of the ground station;

transitioning the aerial vehicle from the hover-flight orientation to a forward-flight orientation, such that a tension of the tether is reduced, wherein the aerial vehicle has attached flow; and

operating the aerial vehicle in the forward-flight orientation to ascend at an angle of ascent to a second location that is on the tether sphere, wherein the second location is downwind of the ground station.

12. The method of claim 11 , wherein operating the aerial vehicle in the forward-flight orientation to ascend at the angle of ascent to the second location comprises selecting a maximum angle of ascent, such that the aerial vehicle has attached flow during the ascent.

13. The method of claim 12 , wherein operating the aerial vehicle in the forward-flight orientation to ascend at the angle of ascent to the second location comprises adjusting a pitch angle of the aerial vehicle based on the maximum angle of ascent.

14. The method of claim 11 , wherein operating the aerial vehicle in the forward-flight orientation to ascend at the angle ascent to the second location comprises operating the aerial vehicle along a portion of the tether sphere.

15. The method of claim 11 , further comprising transitioning the aerial vehicle from the forward-flight orientation to a crosswind-flight orientation.

16. A system comprising:

a tether connected to a ground station, wherein the tether defines a tether sphere having a radius based on a length of the tether;

an aerial vehicle connected to the tether; and

a control system programmed to:

operate the aerial vehicle in a hover-flight orientation;

while the aerial vehicle is in the hover-flight orientation, position the aerial vehicle at a first location that is on the tether sphere, wherein the first location is downwind of the ground station;

transition the aerial vehicle from the hover-flight orientation to a forward-flight orientation, such that a tension of the tether is reduced, wherein the aerial vehicle has attached flow; and

operate the aerial vehicle in the forward-flight orientation to ascend at an angle of ascent to a second location that is on the tether sphere, wherein the second location is downwind of the ground station.

17. The system of claim 16 , wherein the control system is further programmed to select a maximum angle of ascent, such that the aerial vehicle has attached flow during the ascent.

18. The system of claim 16 , wherein the control system is further programmed to operate the aerial vehicle in the forward-flight orientation along a portion of the tether sphere.

19. The system of claim 16 , wherein the control system is further programmed to operate the aerial vehicle in the hover-flight orientation, such that a bottom of the tether remains above a first predetermined altitude,

wherein the control system is further programmed to, while the aerial vehicle is in the hover-flight orientation, position the aerial vehicle at the first location, such that the bottom of the tether remains above a second predetermined altitude,

wherein the control system is further programmed to transition the aerial vehicle from the hover-flight orientation to the forward-flight orientation, such that the bottom of the tether remains above the second predetermined altitude, and

wherein the control system is further programmed to operate the aerial vehicle in the forward-flight orientation to ascend at the angle of ascent to the second location, such that the bottom of the tether remains above the second predetermined altitude.

20. The system of claim 16 , wherein the control system is further programmed to transition the aerial vehicle from the forward-flight orientation to a crosswind-flight orientation.