地磁活动对电离层f0F2月中值的影响与国际参考电离层误差

利用我国9个中低纬度的电离层观测站在1977-1986年间观测的f0F2月中值,按每月的平均地磁活动指数Ap分为地磁活动高（Ap≥5）和低（Ap＜15）两种情况,研究了地磁活动对f0F2月中值平均低纬电离层驼峰区演变的影响,并考察了国际参考电离层（IRI）的误差．     

轴系刚度对新型空气动力负载模拟器的影响

新型空气动力负载模拟器是在传统的电液负载模拟器上增加一个位置同步马达,补偿由舵机主动转动产生的位置扰动。理论和实验研究表明 ,由于同步马达与加载马达之间,舵机马达与加载马达之间不可避免地存在机械连接环节 ,即使同步马达与承载马达完全保持位置同步,加载马达轴和壳的相对速度以及多余力矩也不能百分之百被消除。     

基于ADRC姿态解耦的四旋翼飞行器鲁棒轨迹跟踪

针对欠驱动四旋翼飞行器的控制特性,提出一种基于自抗扰控制(ADRC)的姿态解耦控制算法,该算法可以克服传统欠驱动四旋翼控制方法中存在的问题,如系统状态间耦合严重,抗干扰能力弱及系统建模误差对跟踪性能影响较大等弱点.该算法利用扩张状态观测器(ESO)实现状态间耦合项的跟踪和估计,同时ESO也可实现对系统干扰的估计,干扰包括系统内扰和外扰.利用动态反馈线性化将非线性MIMO系统转化成线性SISO系统,然后利用非线性反馈控制律实现四旋翼姿态系统的高品质控制,在上述姿态解耦控制的基础上研究飞行器的鲁棒轨迹跟踪问题,不同情况下的仿真结果验证了上述姿态控制算法可提高系统轨迹跟踪的鲁棒性.该算法不依赖于精确的系统模型,降低了实际应用的难度,并有很强的抗干扰能力,具有实际应用的价值.      

自抗扰控制技术在电液力伺服系统中的应用

针对无头轧制系统钢坯闪光对焊中顶锻力伺服特性要求,提出了基于自抗扰控制技术及力同步误差反馈校正的复合控制策略.为了更准确地体现所研究电液力伺服系统的非线性、参数时变性以及执行机构的耦合特性,采用AMESim平台进行了系统建模.针对顶锻力伺服的快速大力值加载特性、顶锻过程的变刚度特性、双对接液压缸同步均载要求以及更好地消除系统的其他干扰,设计了基于自抗扰控制技术和比例积分同步误差反馈校正的复合控制策略,以提高系统的鲁棒性、力伺服的快速响应性以及双对接液压缸的同步性能.通过仿真研究,在局部冲击干扰的条件下,仿真结果证实了所提控制策略的有效性和可行性.     

火星着陆器的大气进入段有限时间抗干扰制导律设计

考虑含有外部干扰影响下的火星着陆器的大气进入段制导律设计问题,提出一种基于阻力跟踪的复合制导策略。首先,根据火星着陆器的动力学模型,并结合阻力曲线定义,给出了含有外部干扰的阻力剖线动态方程;其次,为了保证系统有良好的抗干扰性能和较快的跟踪速度,基于阻力剖线动态方程,设计了有限时间反馈制导律;然后,为进一步提高系统的抗干扰能力,设计了干扰观测器,估计未知干扰,利用干扰估计值前馈补偿,最终形成复合制导律。最后,通过对比仿真验证了该方法的有效性和优越性。     

高超声速飞行器抗干扰反步滑模控制

针对存在参数不确定及外部扰动下的高超声速飞行器轨迹跟踪控制问题,研究了一种基于反步法的抗干扰滑模控制设计方法.将非线性高超声速飞行器动力学模型表达为严反馈形式分步进行设计.采用滑模控制方法进行每步的控制器设计,并提出采用扩展状态观测器（ESO,Extended State Observer）方法实现对参数不确定及外部扰动产生的内外干扰进行估计,继而在控制中补偿.扩展状态观测器能保证对干扰的估计收敛到真值附近的邻域内,从而能够保证较好的补偿效果.通过0.5°附加干扰攻角和25%的气动参数偏差下的非线性高超声速飞行器动力学模型仿真结果验证了该抗干扰滑模控制方案对内外干扰的抑制效果和闭环系统良好的跟踪性能.      

Response of the ionospheric F-region in the Brazilian sector during the super geomagnetic storm in April 2000 observed by GPS

The response of the ionospheric F-region in the equatorial and low latitude regions in the Brazilian sector during the super geomagnetic storm on 06–07 April 2000 has been studied in the present investigation. The geomagnetic storm reached a minimum D_st of −288 nT at 0100 UT on 07 April. In this paper, we present vertical total electron content (VTEC) and phase fluctuations (in TECU/min) from GPS observations obtained at Imperatriz (5.5°S, 47.5°W; IMPZ), Brasília (15.9°S, 47.9°W; BRAZ), Presidente Prudente (22.12°S, 51.4°W; UEPP), and Porto Alegre (30.1°S, 51.1°W; POAL) during the period 05–08 April. Also, several GPS-based TEC maps are presented from the global GPS network, showing widespread and drastic TEC changes during the different phases of the geomagnetic storm. In addition, ion density measurements on-board the satellite Defense Meteorological Satellite Program (DMSP) F15 orbiting at an altitude of 840 km and the first Republic of China satellite (ROCSAT-1) orbiting at an altitude of 600 km are presented. The observations indicate that one of the orbits of the DMSP satellite is fairly close to the 4 GPS stations and both the DMSP F15 ion-density plots and the phase fluctuations from GPS observations show no ionospheric irregularities in the Brazilian sector before 2358 UT on the night of 06–07 April 2000. During the fast decrease of D_st on 06 April, there is a prompt penetration of electric field of magnetospheric origin resulting in decrease of VTEC at IMPZ, an equatorial station and large increase in VTEC at POAL, a low latitude station. This resulted in strong phase fluctuations on the night of 06–07 April, up to POAL. During the daytime on 07 April during the recovery phase, the VTEC observations show positive ionospheric storm at all the GPS stations, from IMPZ to POAL, and the effect increasing from IMPZ to POAL. This is possibly linked to the equatorward directed meridional wind. During the daytime on 08 April (the recovery phase continues), the VTEC observations show very small negative ionospheric storm at IMPZ but the positive ionospheric storm effect is observed from BRAZ to POAL possibly linked to enhancement of the equatorial ionospheric anomaly.     

Effects observed in the ionospheric F-region in the South American sector during the intense geomagnetic storm of 14 December 2006

This investigation presents observations related to the generation of equatorial ionospheric irregularities (also known as equatorial spread F (ESF)) including ionospheric plasma bubbles and dynamic behavior of the ionospheric F-region in the South American sector during an intense geomagnetic storm in December 2006 (a period of low solar activity). In this work, ionospheric sounding observations and GPS data obtained between 13 and 16 December 2006 at several stations in the South American sector are presented. On the geomagnetically disturbed night of 14 and 15 December, ionospheric plasma bubbles were observed after an unusual uplifting of the F-region during pre-reversal enhancement (PRE) period. The unusual uplifting of the F-region during PRE was possibly associated with prompt penetration of electric field of magnetospheric origin. During the geomagnetic disturbance night of 14 and 15 December, strong oscillations due to the propagation of traveling ionospheric disturbances (TIDs) by the Joule heating in the auroral region were observed in the F-region at São José dos Campos (SJC, 23.2°S, 45.9°W; dip latitude 17.6°S), Brazil, and Port Stanley (PST, 51.6°S, 57.9°W; geom. latitude 41.6°S). The VTEC-GPS observations presented on the night of 14 and 15 December 2006 show both positive and negative storm phases in the South American sector, possibly due to changes in the large-scale wind circulation and changes in the O/N₂ ratio in the southern hemisphere, respectively.     

低雷诺数下吹吸气射流对NACA0012翼型气动性能的影响

基于Favre过滤的大涡模拟方法,对雷诺数Re=10^4,迎角α=6°下的NACA0012翼型上表面吹吸气射流进行了数值模拟,从翼型周围流场流线图、速度场云图、上下表面压力系数曲线以及上表面边界层位移厚度等多角度地分析了射流位置以及速度变化对翼型气动性能的影响。结果表明:射流位置对翼型气动性能影响较大,且吸气射流要明显优于吹气射流。对于吸气射流,前缘吸气要明显优于中后缘吸气,可有效增升减阻,并减小翼型尾部流动分离,抑制翼型气动参数扰动,其最佳吸气位置随着速度的增大逐渐向下游移动;而吹气射流对翼型气动系数的作用效果较差,但中后缘的吹气射流可减小飞行过程中的气动扰动量,且吹气越大,效果越明显。     

基于新型积分自适应滑模控制策略的永磁同步电机控制

设计了一种永磁同步电机(PMSM)参数扰动和负载扰动的新型控制策略。通常PMSM控制是通过PI控制设计的,控制效果不佳,因此提出一种新型积分滑模控制(SMC)策略进行转速控制器设计。积分SMC具有较强的抗干扰性,不仅可以抑制控制系统的高频微分扰动,而且可以降低系统稳态误差,使控制更精确。设计趋近律函数对滑模控制器进行优化,使SMC参数自适应调节,提高系统响应速度。考虑到系统参数和负载扰动对控制性能的影响,将自抗扰环节引入SMC,提高了系统的抗扰性。最后通过仿真试验验证了控制系统良好的控制性能。