초록 ▼

The present invention is to prevent an uninhabited airborne vehicle from crashing due to fall impact and from being damaged and to protect an object and a living being at the fall point. The uninhabited airborne vehicle 100 includes a rotary wing 10 and a buffer 111 that reduces impact on the airfra

The present invention is to prevent an uninhabited airborne vehicle from crashing due to fall impact and from being damaged and to protect an object and a living being at the fall point. The uninhabited airborne vehicle 100 includes a rotary wing 10 and a buffer 111 that reduces impact on the airframe when crashed. The battery charge remaining measurement module 122 and the distance measurement module 123 measure the battery charge remaining and the distance to an object, respectively, and compare the measurement with the respective thresholds. If the measurement is less than the respective thresholds, the buffer module 111 is driven by the drive module 121.

대표청구항 ▼

1. An uninhabited airborne vehicle comprising: a rotary wing;an airframe;a buffer that reduces impact on the airframe when crashed;a battery charge remaining meter that measures battery charge remaining of the uninhabited airborne vehicle;a moving velocity meter that measures a moving velocity of th

1. An uninhabited airborne vehicle comprising: a rotary wing;an airframe;a buffer that reduces impact on the airframe when crashed;a battery charge remaining meter that measures battery charge remaining of the uninhabited airborne vehicle;a moving velocity meter that measures a moving velocity of the uninhabited airborne vehicle when the battery charge remaining is less than a first threshold; anda driver that drives the buffer when the battery charge remaining is less than the first threshold and the moving velocity is greater than a second threshold while the uninhabited airborne vehicle is flying. 2. The uninhabited airborne vehicle according to claim 1, wherein the driver does not drive the buffer when the uninhabited airborne vehicle makes a landing by a landing instruction from an operator. 3. The uninhabited airborne vehicle according to claim 1, wherein the driver does not drive the buffer when the moving velocity is less than the second threshold. 4. The uninhabited airborne vehicle according to claim 1, wherein the buffer has a form to wrap the uninhabited airborne vehicle. 5. The uninhabited airborne vehicle according to claim 1, further comprising a distance meter that measures a distance between the uninhabited airborne vehicle and an object when the battery charge remaining is greater than the first threshold, wherein the driver drives the buffer when the battery charge remaining is greater than the first threshold and the distance is less than a third threshold while the uninhabited airborne vehicle is flying. 6. The uninhabited airborne vehicle according to claim 5, wherein the distance meter removes frequency noise caused by the rotary wing of the uninhabited airborne vehicle while measuring the distance between the uninhabited airborne vehicle and the object. 7. The uninhabited airborne vehicle according to claim 5, wherein the distance meter checks whether a landing instruction has been received from an operator when the distance is greater than the third threshold, and wherein the uninhabited airborne vehicle makes a landing by the landing instruction when the landing instruction has been received. 8. The uninhabited airborne vehicle according to claim 1, further comprising a distance meter that measures a distance between the uninhabited airborne vehicle and an object when the battery charge remaining is greater than the first threshold, wherein the moving velocity meter measures the moving velocity of the uninhabited airborne vehicle when the battery charge remaining is greater than the first threshold and the distance is less than a third threshold, andwherein the driver drives the buffer when the battery charge remaining is less than the first threshold, the distance is less than the third threshold, and the moving velocity is greater than the second threshold while the uninhabited airborne vehicle is flying. 9. A method of controlling an uninhabited airborne vehicle including a rotary wing, an airframe, and a buffer for reducing impact on the airframe when the uninhabited airborne vehicle is crashed, the method comprising: measuring battery charge remaining of the uninhabited airborne vehicle;measuring a moving velocity of the uninhabited airborne vehicle when the battery charge remaining is less than a first threshold; anddriving the buffer when the battery charge remaining is less than the first threshold and the moving velocity is greater than a second threshold while the uninhabited airborne vehicle is flying. 10. The method according to claim 9, further comprising: measuring a distance between the uninhabited airborne vehicle and an object when the battery charge remaining is greater than the first threshold; anddriving the buffer when the battery charge remaining is greater than the first threshold and the distance is less than a third threshold while the uninhabited airborne vehicle is flying. 11. The method according to claim 10, further comprising: checking whether a landing instruction from an operator has been received when the distance is greater than the third threshold; andallowing the uninhabited airborne vehicle to make a landing by the landing instruction when the landing instruction has been received. 12. The method according to claim 10, further comprising removing frequency noise caused by the rotary wing of the uninhabited airborne vehicle while measuring the distance between the uninhabited airborne vehicle and the object. 13. The method according to claim 9, further comprising: measuring a distance between the uninhabited airborne vehicle and an object when the battery charge remaining is greater than the first threshold;measuring the moving velocity of the uninhabited airborne vehicle when the battery charge remaining is greater than the first threshold and the distance is less than a third threshold; anddriving the buffer when the battery charge remaining is less than the first threshold, the distance is less than the third threshold, and the moving velocity is greater than the second threshold while the uninhabited airborne vehicle is flying. 14. The method according to claim 9, wherein the buffer is not driven when the uninhabited airborne vehicle makes a landing by a landing instruction from an operator. 15. The method according to claim 9, wherein the buffer is not driven when the moving velocity is less than the second threshold. 16. The method according to claim 9, wherein the buffer has a form to wrap the uninhabited airborne vehicle.