To design the control system for some homing missile so that the autopilot can transfer guidance command correctly and be robust to disturbances, such as the measurement noises and parameter variation caused by areody...To design the control system for some homing missile so that the autopilot can transfer guidance command correctly and be robust to disturbances, such as the measurement noises and parameter variation caused by areodynamic floating. The model reference adaptive control was combined with the variable structure control to design a model reference variable structure (MRVS) control system whose control structure is simple and can be realized easily. The simulation results indicate that MRVS can complete the task of transferring guidance command and suppress the distrubances effectively.展开更多
The first integrals and their conditions of existence for variable massnonholonomic system in noninertial relerence frames are obtained,and the canonicalequations and the variation equations of the system are extended...The first integrals and their conditions of existence for variable massnonholonomic system in noninertial relerence frames are obtained,and the canonicalequations and the variation equations of the system are extended. It is proved that using the first integral we can construct the integral invariant of the system.Finally,a series of deductions and an example are given.展开更多
This paper presents a fully on-chip NMOS low-dropout regulator（LDO） for portable applications with quasi floating gate pass element and fast transient response.The quasi floating gate structure makes the gate of the...This paper presents a fully on-chip NMOS low-dropout regulator（LDO） for portable applications with quasi floating gate pass element and fast transient response.The quasi floating gate structure makes the gate of the NMOS transistor only periodically charged or refreshed by the charge pump,which allows the charge pump to be a small economical circuit with small silicon area.In addition,a variable reference circuit is introduced enlarging the dynamic range of error amplifier during load transient.The proposed LDO has been implemented in a 0.35 μm BCD process.From experimental results,the regulator can operate with a minimum dropout voltage of 250 mV at a maximum 1 A load and Iq of 395 μA.Under full-range load current step,the voltage undershoot and overshoot of the proposed LDO are reduced to 50 and 26 mV,respectively.展开更多
文摘To design the control system for some homing missile so that the autopilot can transfer guidance command correctly and be robust to disturbances, such as the measurement noises and parameter variation caused by areodynamic floating. The model reference adaptive control was combined with the variable structure control to design a model reference variable structure (MRVS) control system whose control structure is simple and can be realized easily. The simulation results indicate that MRVS can complete the task of transferring guidance command and suppress the distrubances effectively.
文摘The first integrals and their conditions of existence for variable massnonholonomic system in noninertial relerence frames are obtained,and the canonicalequations and the variation equations of the system are extended. It is proved that using the first integral we can construct the integral invariant of the system.Finally,a series of deductions and an example are given.
文摘This paper presents a fully on-chip NMOS low-dropout regulator（LDO） for portable applications with quasi floating gate pass element and fast transient response.The quasi floating gate structure makes the gate of the NMOS transistor only periodically charged or refreshed by the charge pump,which allows the charge pump to be a small economical circuit with small silicon area.In addition,a variable reference circuit is introduced enlarging the dynamic range of error amplifier during load transient.The proposed LDO has been implemented in a 0.35 μm BCD process.From experimental results,the regulator can operate with a minimum dropout voltage of 250 mV at a maximum 1 A load and Iq of 395 μA.Under full-range load current step,the voltage undershoot and overshoot of the proposed LDO are reduced to 50 and 26 mV,respectively.
