Homeostatic flying hovercraft
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[0096]FIG. 11 depicts a first embodiment of the stabilizer circuit for the hovercraft 10. The XY axis mercury tilt switch stabilizer transducers 52 are linked electrically to the appropriate circuit for roll and pitch correction. For example, the N and S transducers 64 provide status information with regard to pitch actuation 104 while the E and W transducers 64 provide status information with regard to roll actuation 106.
[0097]FIG. 12 shows a block diagram for enable from the X stabilizer circuit or the Y stabilizer circuit to the piezo gyros 56. FIG. 13 shows a schematic diagram of the control system for the motor controllers 58 incorporating the outputs of the stabilizer circuits 52 and the gyro circuits 56. For example, voltage adder 108 computes inputs from Xgyro A, Xstab A, Zgyro A, and Vu / d. Voltage to frequency converters 110 made up of a 555 timer / op amp circuits convert the combined voltage to a frequency for the respective motor speed controllers 58. FIGS. 14-15 show alt...
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