A method and apparatus for changing a flight path of an air platform. A change for the flight path of the air platform is identified. A weight system associated with the air platform is moved during flight of the air platform such that a center of mass of the air platform changes in a manner that ca
A method and apparatus for changing a flight path of an air platform. A change for the flight path of the air platform is identified. A weight system associated with the air platform is moved during flight of the air platform such that a center of mass of the air platform changes in a manner that causes the flight path of the air platform to change.
대표청구항▼
1. A method for changing a flight path of an air platform, the method comprising: supporting, a weight system in flight via connecting a first line and a second line to an airfoil and the weight system, such that the air platform comprises the weight system and the airfoil, the first line connecting
1. A method for changing a flight path of an air platform, the method comprising: supporting, a weight system in flight via connecting a first line and a second line to an airfoil and the weight system, such that the air platform comprises the weight system and the airfoil, the first line connecting to the airfoil at a first location and a second location, the first location being opposite and diagonal to the second location on the airfoil, and the second line connecting to the airfoil at a third location and a fourth location, the third location being opposite and diagonal to the fourth location on the airfoil;identifying a change for the flight path of the air platform; andmoving the weight system associated with the air platform during flight of the air platform such that a center of mass of the air platform changes in a manner that causes the flight path of the air platform to change via moving the weight system via moving the line via a motor connected to the weight system, such that the motor avoids supporting a load of the weight system. 2. The method of claim 1, wherein the moving the weight system is performed to change the flight path of the air platform to a desired flight path for the air platform. 3. The method of claim 1, wherein the step of identifying the change for the flight path of the air platform comprises: receiving input to change the flight path for the air platform to a desired flight path. 4. The method of claim 3, wherein the step of receiving the input to change the flight path for the air platform to the desired flight path comprises: receiving the input from a remote operator of the air platform. 5. A method for changing a flight path of an air platform, the method comprising: identifying a change for the flight path of the air platform; andmoving a weight system associated with the air platform during flight of the air platform such that a center of mass of the air platform changes in a manner that causes the flight path of the air platform to change via moving a line connected to: the weight system and a motor connected to the weight system, via the motor moving the line such that the motor avoids supporting the weight system, such that a first line connects to an airfoil of the air platform at a first location and a second location, the first location being opposite and diagonal to the second location on the airfoil, and a second line connects to the airfoil at a third location and a fourth location, the third location being opposite and diagonal to the fourth location on the airfoil, and the air platform being selected from one of an aircraft, a paraglider, a glider, a fixed-wing vehicle, a parafoil connected to a payload, a hang glider, and a parafoil wing. 6. A method for changing a flight path of an air platform, the air platform comprising: an airfoil;a weight system;members attached to the weight system;one or more lines connecting the weight system to the airfoil, wherein the one or more lines are connected to the weight system via the members, the members are configured to allow the lines to pass through the members, and each end of each line of the one or more lines is connected to the airfoil such that a first line of the one or more lines connects to the airfoil at a first location and a second location, the first location being opposite and diagonal to the second location on the airfoil, and a second line of the one or more lines connects to the airfoil at a third location and a fourth location, the third location being opposite and diagonal to the fourth location on the airfoil;a motor connected to the weight system and engaging the one or more lines, the motor configured to move a line of the one or more lines while the motor avoids supporting a load of the weight system, andthe method comprising:changing a center of mass of the air platform by moving the weight system relative to the airfoil via moving the line via using the motor and avoiding the motor supporting the load of the weight system. 7. The method of claim 6, wherein moving the weight system relative to the one or more lines moves the weight system relative to the airfoil. 8. The method of claim 7, wherein moving the weight system relative to the airfoil changes the center of mass for the air platform relative to a center of lift for the air platform such that the flight path of the air platform changes with respect to at least one of a pitch axis and a roll axis. 9. The method of claim 6, wherein the members comprise: a first member and a second member, the first member and the second member being at opposite and diagonal locations on the weight system; anda third member and a fourth member, the third member and the fourth member being at opposite and diagonal locations on the weight system. 10. The method of claim 9, wherein: the first line passes through the first member and the second member;the second line passes through the third member and the fourth member; andthe first line and the second line form an X-shape over the weight system. 11. The method of claim 6, further comprising the motor engaging the one or more lines. 12. The method of claim 11, wherein the motors include one or more gears that engage one or more chain sections of the one or more lines. 13. The method of claim 12, wherein moving the weight system relative to the one or more lines comprises rotation of the gears by the motors. 14. The method of claim 6, further comprising one or more pulleys connected to the weight system such that the one or more lines pass through grooves in the pulleys; and moving the weight system relative to the one or more lines comprises turning wheels of the pulleys using the motors. 15. The method of claim 6, further comprising a track system connected to the weight system; the one or more lines comprising chains comprising teeth engaging one or more tracks of the track system; andmoving the weight system relative to the one or more lines comprises moving the track using the motors. 16. The method of claim 6, wherein the weight system is a payload for the air platform. 17. The method of claim 6, wherein the members comprise at least one of eyelets, eyelet screws, pulleys, sprockets, gears, or wheels. 18. The method of claim 6, further comprising threading each of the first line and the second line through two members formed as eyelets that are at opposite and diagonal locations on the weight system.
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이 특허에 인용된 특허 (7)
Schwarzler, Hans-Jurgen, Actuation system and method for a load-bearing paraglider.
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