早期近距离无线通信技术(near field communication,NFC)标准规定13.56 MHz无线通信卡的数据速率最高到848 Kbps,在智能手机NFC技术广泛应用的背景下,通信要求达到超高数据速率(very high bit rate,VHBR)。近场通信卡(proximity integra...早期近距离无线通信技术(near field communication,NFC)标准规定13.56 MHz无线通信卡的数据速率最高到848 Kbps,在智能手机NFC技术广泛应用的背景下,通信要求达到超高数据速率(very high bit rate,VHBR)。近场通信卡(proximity integrated circuit card,PICC)接收电路数据速率提升的难点主要在于移幅键控法/移频键控法(amplitude-shift keying/phase-shift keying,ASK/PSK)接收器的设计,其在实际应用中受码间串扰(inter-symbol interference,ISI)、功耗、电路复杂度等限制。针对以上问题,提出一种完整的低功耗PICC解调解码电路设计,包含高定时精度的全数字定时恢复电路。设计实现采用标准0.18μm互补金属氧化物半导体(complementary metal oxide semiconductor,CMOS)工艺,实现了147 pJ/bit的能效,可应用于ASK 0.106~3.39 Mbps数据速率通信。展开更多
All long-duration spacecraft in low-earth-orbit are subject to high velocity impacts by meteoroids and space debris. Such impacts are expected to occur at non-normal incidence angles and can cause severe damage to the...All long-duration spacecraft in low-earth-orbit are subject to high velocity impacts by meteoroids and space debris. Such impacts are expected to occur at non-normal incidence angles and can cause severe damage to the spacecraft and its external flight-critical systems and possibly lead to catastrophic failure of the spacecraft. In order to ensure crew safety and proper function of internal and external spacecraft systems, the characteristics of a debris cloud generated by such impacts must be known. An analytical model is therefore developed for the characterization of the penetration and ricochet debris clouds created by the hypervelocity impact of an aluminum spherical projectile on an aluminum plate. This model employs normal and oblique shock wave theory to characterize the penetration and ricochet processes. The prediction results of center-of-mass trajectory and leading velocity of penetration and ricochet debris clouds are obtained and compared with numerical and experimental results in figures.展开更多
文摘早期近距离无线通信技术(near field communication,NFC)标准规定13.56 MHz无线通信卡的数据速率最高到848 Kbps,在智能手机NFC技术广泛应用的背景下,通信要求达到超高数据速率(very high bit rate,VHBR)。近场通信卡(proximity integrated circuit card,PICC)接收电路数据速率提升的难点主要在于移幅键控法/移频键控法(amplitude-shift keying/phase-shift keying,ASK/PSK)接收器的设计,其在实际应用中受码间串扰(inter-symbol interference,ISI)、功耗、电路复杂度等限制。针对以上问题,提出一种完整的低功耗PICC解调解码电路设计,包含高定时精度的全数字定时恢复电路。设计实现采用标准0.18μm互补金属氧化物半导体(complementary metal oxide semiconductor,CMOS)工艺,实现了147 pJ/bit的能效,可应用于ASK 0.106~3.39 Mbps数据速率通信。
文摘All long-duration spacecraft in low-earth-orbit are subject to high velocity impacts by meteoroids and space debris. Such impacts are expected to occur at non-normal incidence angles and can cause severe damage to the spacecraft and its external flight-critical systems and possibly lead to catastrophic failure of the spacecraft. In order to ensure crew safety and proper function of internal and external spacecraft systems, the characteristics of a debris cloud generated by such impacts must be known. An analytical model is therefore developed for the characterization of the penetration and ricochet debris clouds created by the hypervelocity impact of an aluminum spherical projectile on an aluminum plate. This model employs normal and oblique shock wave theory to characterize the penetration and ricochet processes. The prediction results of center-of-mass trajectory and leading velocity of penetration and ricochet debris clouds are obtained and compared with numerical and experimental results in figures.
