Servo-type phase-locked loop anti-skid brake control system
AssigneeNational Science Council
InventorsEdge C. Yeh, Jiunn Y. Wang
Life of this patent
Estimating the term…
Loading patent…
AssigneeNational Science Council
InventorsEdge C. Yeh, Jiunn Y. Wang
Estimating the term…
An anti-skid brake control system (ABS) utilizing a phase-locked loop (PLL) for controlling the brake mechanism of a landing aircraft. The PLL control system tracks the angular velocity of the nose wheel of the aircraft as a reference signal for locking the angular velocity of the main wheel of the aircraft such that the wheel slip is maintained at a constant value. The PLL control system has a phase detector which takes the signals from both wheel speed detectors and is capable of generating accordingly a frequency error signal and a phase error signal. A circuit will generate an electrical signal, the magnitude of the electrical signal being in accordance with the magnitude of the frequency error signal and the magnitude of the phase error signal. A driving member will drive in accordance with the magnitude of the electrical signal the brake mechanism connected to the main wheel to apply a brake force thereto. The main wheel thus braked will cause the aircraft to be decelerated, the deceleration of the aircraft in turn cause the angular speed of the nose wheel and the main wheel to be slowed down. The slowed-down speeds are in turn detected by the wheel detectors and thus forming a feedback loop.
An anti-skid brake control system for controlling brake mechanisms of a vehicle, the vehicle having at least a first wheel and at least a second wheel, when braking the vehicle the brake mechanisms applying a brake force to the second wheel and the first wheel being under free rolling, the brake control system comprising:
Dependencies are inferred from the claim text.