Design of Pulse Amplitude Modulation Controller for the Attitude Control of the Payload of a Sounding Rocket

과학로켓 탑재부 자세제어를 위한 펄스 진폭 변조 제어기 설계

  • Published : 2000.11.01

Abstract

A pulse amplitude modulation(PAM) controller is designed for the 3 axis attitude control of a sounding rocket. a certain number of fixed level of thrust are used for the pulse amplitude modulation and the nonlinearity of the controller is considered to examine the existence of the limit cycles and the stability analysis is carried out with the aid of Nyquist plot.

Keywords

References

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