This invention pertains to control methods and systems designed to reduce the startup time of gyroscopes, specifically MEMS gyroscopes, used in various electronic and mechanical devices. Traditional gyroscopes, which rely on Automatic Gain Control (AGC) and Phase-Locked Loop (PLL) circuits, suffer from relatively long startup times, delaying the measurement of angular rates and increasing energy consumption. This invention introduces a pulse controller that works in conjunction with the AGC and PLL circuits to accelerate the startup process. The pulse controller emits a signal that, when combined with the input control drive signal, quickly excites the proof mass of the gyroscope, enabling it to reach its steady-state oscillation frequency and amplitude in a shorter time. This method prevents overshooting of the oscillation amplitude, ensuring the gyroscope operates efficiently and safely. The reduced startup time promotes energy efficiency and enhances the performance of devices that require rapid and accurate angular rate measurements, such as smartphones, aircraft, and vehicles. The proposed solution is easily integrable with existing gyroscope control systems, offering a cost-effective and flexible enhancement to current technology.