Title:
MODEL AIRCRAFT CONTROL AND RECEIVING DEVICE
Document Type and Number:
WIPO Patent Application WO/2010/089072
Kind Code:
A3
Abstract:
The invention relates to a model aircraft control and receiving device in a housing (1), comprising an electronic, gyroscopic multi-axis programmable flight attitude controller, in particular a helicopter 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 the housing of the flight attitude controller. The invention further relates to a method in which a model helicopter is controlled and stabilized using the model aircraft control and receiving device described above, 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 aid function.
Inventors:
ROEHR ULRICH (DE)
Application Number:
PCT/EP2010/000596
Publication Date:
November 25, 2010
Filing Date:
February 02, 2010
Export Citation:
Assignee:
MIKADO MODEL HELICOPTERS GMBH (DE)
ROEHR ULRICH (DE)
ROEHR ULRICH (DE)
International Classes:
A63H30/04; A63H27/133
Foreign References:
| US20040245378A1 | 2004-12-09 | |||
| DE3437297A1 | 1986-04-17 | |||
| DE29810356U1 | 1998-08-13 | |||
| DE29805401U1 | 1998-07-02 |
Attorney, Agent or Firm:
RÖHR, Ulrich (Hanau, DE)
Download PDF:
Previous Patent: DRIVE SYSTEM, METHOD FOR OPERATING A DRIVE SYSTEM, AND USE THEREOF
Next Patent: SPINDLE MOTOR
Next Patent: SPINDLE MOTOR