Model helicopter attitude control and receiving device with reduced size and self-learning features
First Claim
1. A model helicopter control and receiving device for controlling a model helicopter wherein the model helicopter comprises at least a tail, a tail rotor for controlling yaw of the model helicopter, a main rotor, and a swashplate for controlling the main rotor to control both pitch and roll of the model helicopter, the device comprising:
- a housing disposed within a fuselage of the model helicopter;
at least one RC receiver module disposed inside said housing and configured to receive a plurality of control signals including one or more swashplate control signals carried on a plurality of control channels, including a plurality of user input instruction signals comprising information corresponding to a plurality of user input instructions, each instruction designated to instruct one of a plurality of mechanisms for controlling at least one aspect of the remote controlled model helicopter, the at least one RC receiver module comprising at least one output;
an electronic, gyroscopic multi-axis programmable flight attitude controller disposed inside said housing, having;
at least one input for receiving the at least one RC receiver module output comprising said plurality of control channels,a plurality of inputs for receiving a plurality of gyroscope signals comprising at least one tail sensor signal and one or more swashplate sensor signals,a processor capable of processing said plurality of control channel signals and said at least one tail sensor and one or more swashplate sensor gyroscope signals, said processor programmed with one or more control algorithms for generating output instructions, comprising a tail control algorithm coupled to a swashplate control algorithm for controlling flight of the model helicopter, wherein the swashplate control algorithm and the tail control algorithm share the one or more swashplate control signals and at least said at least one tail sensor and one or more swashplate sensor gyroscopic signals, model helicopter velocity, yaw rate and tail thrust information; and
an electrical line connecting said at least one RC receiver module output to said at least one input on said controller for receiving said output, said electrical line comprising one signal line, said electrical line configured to combine said plurality of control channels on the one signal line.
1 Assignment
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Accused Products
Abstract
A model aircraft control and receiving device in a housing, comprising an electronic, gyroscopic multi-axis programmable flight attitude controller, having control inputs for a plurality of control channels and inputs for gyroscope signals, wherein the flight attitude controller provides at least one input for a receiver module disposed inside or outside of the housing of the flight attitude controller. The device may be used in a method for controlling and stabilizing a model helicopter, wherein the control comprises a self-learning function and/or the control comprises a coupling of the tail controller to the swashplate controller and/or the control comprises a stopping support function.
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Citations
15 Claims
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1. A model helicopter control and receiving device for controlling a model helicopter wherein the model helicopter comprises at least a tail, a tail rotor for controlling yaw of the model helicopter, a main rotor, and a swashplate for controlling the main rotor to control both pitch and roll of the model helicopter, the device comprising:
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a housing disposed within a fuselage of the model helicopter; at least one RC receiver module disposed inside said housing and configured to receive a plurality of control signals including one or more swashplate control signals carried on a plurality of control channels, including a plurality of user input instruction signals comprising information corresponding to a plurality of user input instructions, each instruction designated to instruct one of a plurality of mechanisms for controlling at least one aspect of the remote controlled model helicopter, the at least one RC receiver module comprising at least one output; an electronic, gyroscopic multi-axis programmable flight attitude controller disposed inside said housing, having; at least one input for receiving the at least one RC receiver module output comprising said plurality of control channels, a plurality of inputs for receiving a plurality of gyroscope signals comprising at least one tail sensor signal and one or more swashplate sensor signals, a processor capable of processing said plurality of control channel signals and said at least one tail sensor and one or more swashplate sensor gyroscope signals, said processor programmed with one or more control algorithms for generating output instructions, comprising a tail control algorithm coupled to a swashplate control algorithm for controlling flight of the model helicopter, wherein the swashplate control algorithm and the tail control algorithm share the one or more swashplate control signals and at least said at least one tail sensor and one or more swashplate sensor gyroscopic signals, model helicopter velocity, yaw rate and tail thrust information; and an electrical line connecting said at least one RC receiver module output to said at least one input on said controller for receiving said output, said electrical line comprising one signal line, said electrical line configured to combine said plurality of control channels on the one signal line. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15)
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Specification