IP Library Granted Patent US 10,683,086
Granted Patent B2
US 10,683,086 · App. 15/558,058 · Granted Jun 16, 2020

Unmanned rotorcraft and method for measuring circumjacent object around rotorcraft

Inventor: Kazuo Ichihara (Nagoya, JP)
Assignee: PRODRONE CO., LTD.
B64C27/08B64C25/32B64C39/024B64D45/04B64D47/08B64C2025/325B64C2201/027B64C2201/108B64C2201/14B64D45/08
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Quick Facts
Patent No.
US 10,683,086
App. No.
15/558,058
Granted
Jun 16, 2020
Kind
B2
Abstract

To provide an unmanned rotorcraft and a method for measuring a distance to a circumjacent objet around the rotorcraft, enabling it to prevent its airframe from colliding with a circumjacent object when flying and prevent its airframe from falling down when landing, while suppressing an increase in airframe cost. This is solved by an unmanned rotorcraft including a distance sensor to measure a distance between its airframe and a circumjacent object around it, the distance sensor and its detection direction being fixed to the airframe, and a method for measuring a distance to a circumjacent objet around the rotorcraft, adapted to watch or watch out for a circumjacent object around the airframe by turning the airframe automatically in a yaw direction under predefined conditions or to measure a difference of elevation at landing points of all legs of the airframe.

Claims (28)

1. An unmanned rotorcraft comprising:

an airframe;

a plurality of arms that radially extend from the airframe;

a plurality of skids that extend downward, wherein each skid of the plurality of skids is attached to the airframe via a respective arm of the plurality of arms;

at least one distance sensor to measure a distance between the airframe and a circumjacent object around the airframe, wherein the at least one distance sensor and a detection direction of the at least one distance sensor are fixed to the airframe via an arm of the plurality of arms; and

a controller that is configured to turn the airframe automatically in a yaw direction under predefined conditions to orient the at least one distance sensor toward a plurality of different orientations or positions,

wherein some arms of the plurality of arms are not provided with a distance sensor of the at least one distance sensor.

2. The unmanned rotorcraft according to claim 1 , wherein the controller turns the airframe in predetermined angle steps according to a detection angle of the at least one distance sensor.

3. The unmanned rotorcraft according to claim 1 , wherein the controller turns the airframe continuously.

4. The unmanned rotorcraft according to claim 1 , wherein, when the airframe is flying horizontally, the controller turns the airframe so as to orient the at least one distance sensor along a direction of movement of the airframe and, additionally, orient the at least one distance sensor toward a direction differing from the direction of movement of the airframe at a predetermined period and by a predetermined angle.

5. The unmanned rotorcraft according to claim 1 , wherein the controller:

when the at least one distance sensor has detected a circumjacent object, stores in a memory a position of the circumjacent object as a circumjacent object to watch out for;

calculates a predicted time of collision with the circumjacent object based on a flying speed of the airframe and the position of the circumjacent object when the detected circumjacent object is not stored as the circumjacent object to watch out for, and

calculates a predicted time of collision with the circumjacent object based on a relative approach speed between the airframe and the circumjacent object and the position of the circumjacent object when the detected circumjacent object is stored as the circumjacent object to watch out for.

6. The unmanned rotorcraft according to claim 1 , further comprising:

a plurality of legs to support the airframe when the airframe lands, wherein:

the at least one distance sensor is installed in a position and orientation in order to measure a distance between at least one of the legs and a landing point, and

the controller turns the airframe near the landing point and measures a distance to the landing point for all the legs.

7. The unmanned rotorcraft according to claim 6 , wherein the controller displaces the airframe in a horizontal direction when a difference in distances from the respective legs to the landing point measured by the controller is more than a predetermined value.

8. A method for measuring a distance to a circumjacent object around an unmanned rotorcraft, wherein the unmanned rotorcraft includes an airframe, a plurality of arms that radially extend from the airframe, a plurality of skids that extend downward, wherein each skid of the plurality of skids is attached to the airframe via a respective arm of the plurality of arms, at least one distance sensor to measure a distance between an airframe and a circumjacent object around the airframe, and the at least one distance sensor and a detection direction of the at least one distance sensor are fixed to the airframe via an arm of the plurality of arms, the method comprising:

watching for an approaching object to detect a circumjacent object all around the airframe by automatically turning the airframe around entirely in a yaw direction under predefined conditions,

wherein some arms of the plurality of arms are not provided with a distance sensor of the at least one distance sensor.

9. A method for measuring a distance to a circumjacent object around an unmanned rotorcraft, wherein the unmanned rotorcraft includes an airframe, a plurality of arms that radially extend from the airframe, a plurality of skids that extend downward, wherein each skid of the plurality of skids is attached to the airframe via a respective arm of the plurality of arms, at least one distance sensor to measure a distance between an airframe and a circumjacent object around the airframe, and the at least one distance sensor and a detection direction are fixed to the airframe, the method comprising:

watching for an obstacle to turn the airframe so as to orient the at least one distance sensor along a direction of movement of the airframe and, additionally, orient the at least one distance sensor toward a direction differing from the direction of movement of the airframe at a predetermined period and by a predetermined angle when the airframe is flying horizontally,

wherein some arms of the plurality of arms are not provided with a distance sensor of the at east one distance sensor.

10. A method for measuring a distance to a circumjacent object around an unmanned rotorcraft, wherein the unmanned rotorcraft includes: an airframe, a plurality of arms that radially extend from the airframe, at least one distance sensor to measure a distance between an airframe and a circumjacent object around the airframe; and a plurality of legs to support the airframe when the airframe lands, and the at least one distance sensor is installed in a position and orientation in a portion of the plurality of legs, making it possible to measure a distance between at least one of the legs and a landing point, the method comprising:

detecting a difference of elevation to measure a distance to the landing point for all the legs by turning the airframe near the landing point,

wherein some legs of the plurality of legs are not provided with a distance sensor of the at least one distance sensor.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 13, 2017
From: ICHIHARA, KAZUO
To: PRODRONE CO., LTD.
Reel/Frame 043577/0423 →
Priority Claims (1)
JP 2015-056957 · Mar 19, 2015 · national
Continuity (1)
Related Publication 20180065735A1 · Mar 8, 2018