Autonomous control method for a small, unmanned helicopter
First Claim
1. An autonomous control program for a small unmanned helicopter wherein the program detects the current position, the attitude angle, the altitude relative to the ground, and the absolute azimuth of the nose of the small unmanned helicopter;
- establishes position or velocity reference values from the ground station;
determines optimal control reference values for driving the servo motors that move a number of helicopter rudders from the current position and attitude angle of said small unmanned helicopter detected by said sensors;
based upon said computational processing results, effects translational motion control and tri-axial orientation control on the small unmanned helicopter;
or defines the mathematical model for transfer function representation including pitching operation input and pitch axis attitude angles in the tri-axial orientation control for said small unmanned helicopter as and based upon said model equations, causes said primary computational unit to calculate optimal control reference values for driving the servo motors.
1 Assignment
0 Petitions
Accused Products
Abstract
An objective of the present invention is to provide an autonomous control method that autonomously controls a small unmanned helicopter toward target values, such as a set position and velocity, by deriving model formulas that are well suited for the autonomous control of small unmanned helicopters, by designing an autonomous control algorithm based on the model formulas, and by calculating the autonomous control algorithm.
The autonomous control system for a small unmanned helicopter of the present invention comprises: sensors that detect the current position, the attitude angle, the altitude relative to the ground, and the absolute azimuth of the nose of the aforementioned small unmanned helicopter; a primary computational unit that calculates optimal control reference values for driving the servo motors that move five rudders on the helicopter from target position or velocity values that are set by the ground station and the aforementioned current position and attitude angle of the small unmanned helicopter that are detected by the aforementioned sensors; an autonomous control system equipped with a secondary computational unit that converts the data collected by said sensors and the computational results as numeric values that are output by said primary computational unit into pulse signals that can be accepted by the servo motors, such that these components are assembled into a small frame box, thereby achieving both size and weight reductions;
a ground station host computer that can also be used as the aforementioned computational unit for the aforementioned autonomous control system;
if the aforementioned ground station host computer is used as the aforementioned computational unit for the aforementioned autonomous control system,
in the process of directing the computational results that are output from said ground station host computer to said servo motors through a manual operation transmitter, a radio control generator that converts said computational results as numerical values into pulse signals that said manual operation transmitter can accept;
a servo pulse mixing/switching apparatus, on all said servo motors for said small unmanned helicopter, that permits the switching of manual operation signals and said control signals that are output from said autonomous control system or mixing thereof in any ratio;
an autonomous control algorithm wherein the mathematical model for transfer function representation encompassing pitching operation input through pitch axis attitude angles in the tri-axis orientation control for said small unmanned helicopter is defined as
such that the aforementioned small unmanned helicopter is controlled autonomously based on the aforementioned mathematical model;
51 Citations
19 Claims
-
1. An autonomous control program for a small unmanned helicopter wherein the program detects the current position, the attitude angle, the altitude relative to the ground, and the absolute azimuth of the nose of the small unmanned helicopter;
-
establishes position or velocity reference values from the ground station;
determines optimal control reference values for driving the servo motors that move a number of helicopter rudders from the current position and attitude angle of said small unmanned helicopter detected by said sensors;
based upon said computational processing results, effects translational motion control and tri-axial orientation control on the small unmanned helicopter;
ordefines the mathematical model for transfer function representation including pitching operation input and pitch axis attitude angles in the tri-axial orientation control for said small unmanned helicopter as and based upon said model equations, causes said primary computational unit to calculate optimal control reference values for driving the servo motors. - View Dependent Claims (7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19)
-
-
2. An autonomous control program for a small unmanned helicopter wherein the program detects the current position, the attitude angle, the altitude relative to the ground, and the absolute azimuth of the nose of the small unmanned helicopter;
-
establishes position or velocity reference values from the ground station;
determines optimal control reference values for driving the servo motors that move a number of helicopter rudders from the current position and attitude angle of said small unmanned helicopter detected by said sensors;
based upon said computational processing results, effects translational motion control and tri-axial orientation control on the small unmanned helicopter;
ordefines the mathematical model for a transfer function representation including the rolling input and roll axis attitude angles in the tri-axial orientation control for said small unmanned helicopter as and based upon said model equations, causes said primary computational unit to calculate optimal control reference values for driving the servo motors.
-
-
3. An autonomous control method for a small unmanned helicopter wherein the method detects the current position, the attitude angle, the altitude relative to the ground, and the absolute azimuth of the nose of the small unmanned helicopter;
-
establishes position or velocity reference values from the ground station;
determines optimal control reference values for driving the servo motors that move a number of helicopter rudders from the current position and attitude angle of said small unmanned helicopter detected by said sensors;
based upon said computational processing results, effects translational motion control and tri-axial orientation control on the small unmanned helicopter;
ordefines the mathematical model for transfer function representation including yawing input and yawing axis attitude angles in the tri-axial orientation control for said small unmanned helicopter as and based upon said model equations, causes said primary computational unit to calculate optimal control reference values for driving the servo motors.
-
-
4. An autonomous control method for a small unmanned helicopter wherein the method detects the current position, the attitude angle, the altitude relative to the ground, and the absolute azimuth of the nose of the small unmanned helicopter;
-
establishes position or velocity reference values from the ground station;
determines optimal control reference values for driving the servo motors that move a number of helicopter rudders from the current position and attitude angle of said small unmanned helicopter detected by said sensors;
based upon said computational processing results, effects translational motion control and tri-axial orientation control on the small unmanned helicopter;
ordefines the mathematical model for transfer function representation including pitching axis attitude angles and the longitudinal speed in the tri-axial orientation control for said small unmanned helicopter as and based upon said model equations, causes said primary computational unit to calculate optimal control reference values for driving the servo motors.
-
-
5. An autonomous control method for a small unmanned helicopter wherein the method detects the current position, the attitude angle, the altitude relative to the ground, and the absolute azimuth of the nose of a small unmanned helicopter;
-
establishes position or velocity reference values from the ground station;
determines optimal control reference values for driving the servo motors that move a number of helicopter rudders from the current position and attitude angle of said small unmanned helicopter detected by said sensors;
based upon said computational processing results, effects translational motion control and tri-axial orientation control on the small unmanned helicopter;
ordefines the mathematical model for transfer function representation including rolling axis attitude angles and the lateral speed in the translational motion control for said small unmanned helicopter as and based upon said model equations, causes said primary computational unit to calculate optimal control reference values for driving the servo motors.
-
-
6. An autonomous control method for a small unmanned helicopter wherein the method detects the current position, the attitude angle, the altitude relative to the ground, and the absolute azimuth of the nose of the small unmanned helicopter;
-
establishes position or velocity reference values from the ground station;
determines optimal control reference values for driving the servo motors that move a number of helicopter rudders from the current position and attitude angle of said small unmanned helicopter detected by said sensors;
based upon said computational processing results, effects translational motion control and tri-axial orientation control on the small unmanned helicopter;
ordefines the mathematical model for transfer function representation of the vertical speed in the translational motion control for said small unmanned helicopter as and based upon said model equations, causes said primary computational unit to calculate optimal control reference values for driving the servo motors.
-
Specification