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231.
数字景象图的计算机模拟生成 总被引:8,自引:0,他引:8
数字景象图在飞行器末制导中起着关键作用。在特殊情形下,有必要用计算机模拟生成数字景象图。本文在分析数字景象图成象机理的基础上给出了一个基于数字高程图模拟生成数字景象图的框架,分别讨论了光照模型,大气模型,误差模型,坐标系和视点变换等关键步骤。文中给出了模拟生成的结果。 相似文献
232.
去均值归一化模板互相关(ZNCC)是工程中应用最多的图像匹配算法,但过高的计算复杂度严重限制了其在实时系统中的应用.针对这一问题,提出了基于快速哈特莱变换的快速模板图像匹配算法,首先推导了该算法在哈特莱域的表达式,利用可分离的快速哈特莱变换对相关面进行高效率整体计算,然后在空间域对获取的相关面进行快速归一化处理和极值搜索,并通过空间换取时间和积分图的策略进一步加快算法的计算速度.对算法计算量的定量分析和仿真实验结果表明,算法计算效率高,并且可以完全重构,加速比与图像内容无关,综合性能全面优于现有算法,具有良好的工程应用前景. 相似文献
233.
Irma Rodríguez-Pérez Cristina García-Serrano Carlos Catalán Catalán Alvaro Mozo García Patrizia Tavella Lorenzo Galleani Francisco Amarillo 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
A new integrity monitoring mechanisms to be implemented on-board on a GNSS taking advantage of inter-satellite links has been introduced. This is based on accurate range and Doppler measurements not affected neither by atmospheric delays nor ground local degradation (multipath and interference). By a linear combination of the Inter-Satellite Links Observables, appropriate observables for both satellite orbits and clock monitoring are obtained and by the proposed algorithms it is possible to reduce the time-to-alarm and the probability of undetected satellite anomalies. 相似文献
234.
分析了DG-1型多普勒/GPS组合导航系统,在不同工作方式下导航误差所引起的搜索方位角的误差;讨论了由于搜索方位角的变化引起的搜索域的变化。通过对机理的研究提出了解决办法。 相似文献
235.
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High altitude air-launched autonomous underwater vehicle (AL-AUV) is a new anti-submarine field, which is designed on the Lockheed Martin's high altitude anti-submarine warfare weapons concept (HAAWC) and conducts the basic aerodynamic feasibility in a series of wind tunnel trials. The AL-AUV is composed of a traditional torpedo-like AUV, an additional ex-range gliding wings unit and a descending parachute unit. In order to accurately and conveniently investigate the dynamic and static characteristic of high altitude AL-AUV, a simulation platform is established based on MATLAB/SIMULINK and an AUV 6DOF (Degree of Freedom) dynamic model. Executing the simulation platform for different wing's parameters and initial fixing angle, a set of AUV gliding data is generated. Analyzing the recorded simulation result, the velocity and pitch characteristics of AL-AUV deployed at varying wing areas and initial setting angle, the optimal wing area is selected for specific AUV model. Then the comparative simulations of AL-AUV with the selected wings are completed, which simulate the AUV gliding through idealized windless air environment and gliding with Dryden wind influence. The result indicates that the method of wing design and simulation with the simulation platform based on SIMULINK is accurately effective and suitable to be widely employed. 相似文献
238.
Zhouzheng Gao Tuan Li Hongping Zhang Maorong Ge Harald Schuh 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(9):2393-2405
Since China’s BeiDou satellite navigation system (BDS) began to provide regional navigation service for Asia-Pacific region after 2012, more new generation BDS satellites have been launched to further expand BDS’s coverage to be global. In this contribution, precise positioning models based on BDS and the corresponding mathematical algorithms are presented in detail. Then, an evaluation on BDS’s real-time dynamic positioning and navigation performance is presented in Precise Point Positioning (PPP), Real-time Kinematic (RTK), Inertial Navigation System (INS) tightly aided PPP and RTK modes by processing a set of land-borne vehicle experiment data. Results indicate that BDS positioning Root Mean Square (RMS) in north, east, and vertical components are 2.0, 2.7, and 7.6?cm in RTK mode and 7.8, 14.7, and 24.8?cm in PPP mode, which are close to GPS positioning accuracy. Meanwhile, with the help of INS, about 38.8%, 67.5%, and 66.5% improvements can be obtained by using PPP/INS tight-integration mode. Such enhancements in RTK/INS tight-integration mode are 14.1%, 34.0%, and 41.9%. Moreover, the accuracy of velocimetry and attitude determination can be improved to be better than 1?cm/s and 0.1°, respectively. Besides, the continuity and reliability of BDS in both PPP and RTK modes can also be ameliorated significantly by INS during satellite signal missing periods. 相似文献
239.
《中国航空学报》2020,33(11):2825-2827
With the rapid development of Unmanned Aerial Vehicle (UAV) technology, one of the emerging fields is to utilize multi-UAV as a team under autonomous control in a complex environment. Among the challenges in fully achieving autonomous control, Cooperative task assignment stands out as the key function. In this paper, we analyze the importance and difficulties of multi-UAV cooperative task assignment in characterizing scenarios and obtaining high-quality solutions. Furthermore, we present three promising directions for future research: Cooperative task assignment in a dynamic complex environment, in an unmanned-manned aircraft system and in a UAV swarm. Our goal is to provide a brief review of multi-UAV cooperative task assignment for readers to further explore. 相似文献
240.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2020,65(7):1723-1741
This work develops a deep reinforcement learning based approach for Six Degree-of-Freedom (DOF) planetary powered descent and landing. Future Mars missions will require advanced guidance, navigation, and control algorithms for the powered descent phase to target specific surface locations and achieve pinpoint accuracy (landing error ellipse <5 m radius). This requires both a navigation system capable of estimating the lander’s state in real-time and a guidance and control system that can map the estimated lander state to a commanded thrust for each lander engine. In this paper, we present a novel integrated guidance and control algorithm designed by applying the principles of reinforcement learning theory. The latter is used to learn a policy mapping the lander’s estimated state directly to a commanded thrust for each engine, resulting in accurate and almost fuel-optimal trajectories over a realistic deployment ellipse. Specifically, we use proximal policy optimization, a policy gradient method, to learn the policy. Another contribution of this paper is the use of different discount rates for terminal and shaping rewards, which significantly enhances optimization performance. We present simulation results demonstrating the guidance and control system’s performance in a 6-DOF simulation environment and demonstrate robustness to noise and system parameter uncertainty. 相似文献