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1.
几种陆用惯性自寻北方案的比较   总被引:2,自引:1,他引:1  
纪明 《应用光学》1992,13(4):40-44
介绍几种目前广泛应用于军事及民用工业领域的高精度自寻北方案,同时讨论并分析了这些方案的精度和误差补偿方法,提出在兵器领域尤其是在陆用车辆上的适用性等问题。  相似文献   
2.
高职教育的教学计划的制定是一项复杂的工程。教育部长周济在全国高职高专教育产学研会议上的讲话也提出高职高专教育要“以服务为宗旨,以就业为导向”。通过对比后分析,我们认为只有充分利用自身的教学资源.加大实践课的比重,才能办出高职教育的特色来。  相似文献   
3.
浅议高职学生就业指导的几个观念   总被引:1,自引:0,他引:1  
在高职学生就业指导过程中,要牢固树立就业为导向的观念,树立对学生进行心理分析观念,树立大就业观念,树立安全教育第一的观念,有的放矢地帮助学生顺利走上工作岗位。  相似文献   
4.
The application and the performance of the neighboring optimal feedback scheme presented in Part 1 of this paper is demonstrated for the heating-constrained cross-range maximization problem of a space-shuttle-orbiter-type vehicle. This problem contains five state variables, two control variables, and a state variable inequality constraint of order zero.This research was supported in part by the Deutsche Forschungsgemeinschaft under the Schwerpunktprogramm Anwendungsbezogene Optimierung und Steuerung.The authors wish to express their sincere and grateful appreciation to Professor Roland Bulirsch who encouraged this work.  相似文献   
5.
Standard wind identification techniques employed in the analysis of aircraft accidents are post-facto techniques; they are processed after the event has taken place and are based on the complete time histories of the DFDR/ATCR data along the entire trajectory. By contrast, real-time wind identification techniques are processed while the event is taking place; they are based solely on the knowledge of the preceding time histories of the DFDR/ATCR data.In this paper, a real-time wind identification technique is developed. First, a 3D-kinematic approach is employed in connection with the DFDR/ATCR data covering the time interval preceding the present time instant. The aircraft position, inertial velocity, and accelerometer bias are determined by matching the flight trajectory computed from the DFDR data with the flight trajectory available from the ATCR data. This leads to a least-square problem, which is solved analytically every seconds, with / small.With the inertial velocity and accelerometer bias known, an extrapolation process takes place so as to predict the inertial velocity profile over the subsequent -subinterval. At the end of this subinterval, the extrapolated inertial velocity and the newly identified inertial velocity are statistically reconciled and smoothed. Then, the process of identification, extrapolation, reconciliation, and smoothing is repeated. Subsequently, the wind is computed as the difference between the inertial velocity and the airspeed, which is available from the DFDR data. With the wind identified, windshear detection can take place (Ref. 1).As an example, the real-time wind identification technique is applied to Flight Delta 191, which crashed at Dallas-Fort Worth International Airport on August 2, 1985. The numerical results show that the wind obtained via real-time identification is qualitatively and quantitatively close to the wind obtained via standard identification. This being the case, it is felt that real-time wind identification can be useful in windhsear detection and guidance, above all if the shear/downdraft factor signal is replaced by the wind difference signal (Ref. 1).This paper and its companion (Ref. 1) are based on Refs. 2–4.This research was supported by the Aviation Research and Education Foundation and by Texas Advanced Technology Program, Grant No. TATP-003604020.  相似文献   
6.
开展数学探究式教学的必要性已成共识,但教学观察与调研表明,在数学课堂上,大部分学生数学探究精神匮乏、探究能力低下,对探究的策略与方法十分生疏,教师因学生探究费时和教学用时紧张,无法给学生腾出充裕的思考时间。合理开展数学探究式教学,必须正视以上课堂教学实情,依教情时常开展探究示范教学,让学生掌握探究的策略与方法,依学情在学生探究时点拨激励,助其形成主动探索的能力与习惯。  相似文献   
7.
Research suggests that spatial ability may predict success in complex disciplines including anatomy, where mastery requires a firm understanding of the intricate relationships occurring along the course of veins, arteries, and nerves, as they traverse through and around bones, muscles, and organs. Debate exists on the malleability of spatial ability, and some suggest that spatial ability can be enhanced through training. It is hypothesized that spatial ability can be trained in low-performing individuals through visual guidance. To address this, training was completed through a visual guidance protocol. This protocol was based on eye-movement patterns of high-performing individuals, collected via eye-tracking as they completed an Electronic Mental Rotations Test (EMRT). The effects of guidance were evaluated using 33 individuals with low mental rotation ability, in a counterbalanced crossover design. Individuals were placed in one of two treatment groups (late or early guidance) and completed both a guided, and an unguided EMRT. A third group (no guidance/control) completed two unguided EMRTs. All groups demonstrated an increase in EMRT scores on their second test (P < 0.001); however, an interaction was observed between treatment and test iteration (P = 0.024). The effect of guidance on scores was contingent on when the guidance was applied. When guidance was applied early, scores were significantly greater than expected (P = 0.028). These findings suggest that by guiding individuals with low mental rotation ability “where” to look early in training, better search approaches may be adopted, yielding improvements in spatial reasoning scores. It is proposed that visual guidance may be applied in spatial fields, such as STEMM (science, technology, engineering, mathematics and medicine), surgery, and anatomy to improve student's interpretation of visual content. Anat Sci Educ. © 2018 American Association of Anatomists.  相似文献   
8.
目的研究连续臂丛神经阻滞镇痛对断指再植术后再植指血流动力学的影响,探讨其缓解血管痉挛、增加血流量的可行性。方法将60例急诊行断指再植术患者按随机数字表法分为术后连续臂丛神经阻滞镇痛组(CA组)和对照组(NA组),每组30例。观察两组患者再植指术后血管痉挛、血管栓塞和指体坏死发生例数并计算再植指成活率,记录两组术后即刻(T1)、术后24h(T2)再植指固有动脉血流动力学参数及动脉内径(AD)、远指端血氧饱和度(SpO2)和温度(Ts)变化。结果断指再植术后成活率CA组高于NA组,血管痉挛、血管栓塞和指体坏死发生率CA组均低于NA组,差异均有统计学意义(均P<0.05)。在T2时CA组各项血流动力学参数、AD、SpO2、Ts均高于NA组,阻力指数(RI)低于NA组,差异均有统计学意义(均P<0.05)。结论术后连续臂丛神经阻滞镇痛可以缓解再植指固有动脉痉挛,增加指体血流量,提高了断指再植的成功率。  相似文献   
9.
随着经济的发展和改革的不断深化,高校学生参与政治的热情有淡化的趋势。高校学生党支部面临着一系列新的挑战。必须加强党支部的培训和发展工作,改变工作方法,增强党支部的吸引力和凝聚力。  相似文献   
10.
对于采用复合制导的空地导弹,中末制导交接班问题是影响命中概率的关键因素。针对这一问题,采用变结构理论设计中制导律。首先建立滑模面,保证滑模面上速度矢量与视线重合,且零化视线角速率,然后设计到达函数,使到达条件得到满足,可以保证交班时刻导弹可靠捕获目标,并为末制导提供最优初始条件。建立了导弹六自由度数学模型和目标捕获模型,进行全系统数字仿真,实验结果表明:在中末制导交接时刻,弹目视线与导弹速度矢量基本重合,误差为0.12°,视线角速度为-0.02°/s,在±20°视场下满足捕获需求,并且为末制导提供最优初始条件。该方法可以满足中末制导交接班要求,具有较强鲁棒性,且中制导段弹道平滑,需用过载小。  相似文献   
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