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991.
基于GPS/DR的车辆导航系统研究 总被引:4,自引:0,他引:4
张乃镇 《沈阳航空工业学院学报》2001,18(3):7-9
本文研究了GPS和航位推算系统的组合导航技术,给出了GPS/DR组合导航系统的设计方案。由GPS接收机、压电陀螺仪和车载里程仪组成的多传感器系统通过卡尔曼滤波器实现信息融合,以提高GPS/DR组合系统导航精度。同时也对GPS/DR系统的MAP图像处理、软件流程和工程实现做了简要说明。 相似文献
992.
993.
Nikos Mastrodemos Daniel G. Kubitschek Stephen P. Synnott 《Space Science Reviews》2005,117(1-2):95-121
The engineering goal of the Deep Impact mission is to impact comet Tempel 1 on July 4, 2005, with a 370 kg active Impactor
spacecraft (s/c). The impact velocity will be just over 10 km/s and is expected to excavate a crater approximately 20 m deep
and 100 m wide. The Impactor s/c will be delivered to the vicinity of Tempel 1 by the Flyby s/c, which is also the key observing
platform for the event. Following Impactor release, the Flyby will change course to pass the nucleus at an altitude of 500
km and at the same time slow down in order to allow approximately 800 s of observation of the impact event, ejecta plume expansion,
and crater formation. Deep Impact will use the autonomous optical navigation (AutoNav) software system to guide the Impactor
s/c to intercept the nucleus of Tempel 1 at a location that is illuminated and viewable from the Flyby. The Flyby s/c uses
identical software to determine its comet-relative trajectory and provide the attitude determination and control system (ADCS)
with the relative position information necessary to point the High Resolution Imager (HRI) and Medium Resolution Imager (MRI)
instruments at the impact site during the encounter. This paper describes the Impactor s/c autonomous targeting design and
the Flyby s/c autonomous tracking design, including image processing and navigation (trajectory estimation and maneuver computation).
We also discuss the analysis that led to the current design, the expected system performance as compared to the key mission
requirements and the sensitivity to various s/c subsystems and Tempel 1 environmental factors. 相似文献
994.
995.
R.L.C. Starling E.M. Puchnarewicz E. Romero-Colmenero K.O. Mason 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2004,34(12):2588-2593
We present a series of monitoring observations of the ultrasoft broad-line Seyfert galaxy RE J2248-511 with XMM-Newton. Previous X-ray observations showed a transition from a very soft state to a harder state five years later. We find that the ultrasoft X-ray excess has re-emerged, yet there is no change in the hard power-law. Reflection models with a reflection fraction of 15, and Comptonisation models with two components of different temperatures and optical depths (kT1 = 83 keV, T1 = 30 eV, τ1 = 0.8; KT2 = 3.5 keV, T2 = 60 eV, τ2 = 2.8) can be fit to the spectrum, but cannot be constrained. The best representation of the spectrum is a model consisting of two blackbodies (kT1 = 0.09 ± 0.01 keV, kT2 = 0.21 ± 0.03 keV) plus a power-law (Γ = 1.8 ± 0.08). We also present simultaneous optical and infrared data showing that the optical spectral slope also changes dramatically on timescales of years. If the optical to X-ray flux comes primarily from a Comptonised accretion disk we obtain estimates for the black hole mass , accretion rate and inclination cos(i) 0.8 of the disk. 相似文献
996.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2023,71(1):624-644
The integration of geosynchronous orbit (GSO) satellites in Global Navigation Satellite Systems (GNSS) is mostly discussed to enable a regional enhancement for tracking. But how do GSO satellites affect the orbit determination of the rest of the constellation? How accurately can these orbits be determined in a future GNSS tracking scenario with optical links? In this simulation study we analyze the benefit of GSO satellites as an expansion of a MEO (Medium Earth Orbit) satellite constellation – we selected the Galileo satellite constellation – for MEO Precise Orbit Determination (POD). We address not only the impact on POD of MEO satellites but also the possibility to precisely determine the GSO satellites – geostationary orbits (GEO) and inclined geosynchronous orbits (IGSO) – in such an expanded MEO constellation. In addition to GNSS microwave observations, we analyze the influence of different optical links between the participating entities: Optical two-way Inter-Satellite Links (OISL) and ground-space oriented Optical Two-Way Links (OTWL). These optical measurements together with the GNSS microwave observations give a remarkable benefit for the POD capability. In the case of GNSS and OTWL, we simulate the measurements with regard to a network of 16 ground stations. We pay great attention to the simulation of systematic effects of all measurement techniques. We discuss the influence on the systematic errors as well as the formal orbit uncertainties. A MEO constellation expanded with GSO satellites as well as the use of optical links together with GNSS observations not only improves the MEO satellite orbits but also the GSOs to a great extent. 相似文献
997.
Peter W. A. Roming Thomas E. Kennedy Keith O. Mason John A. Nousek Lindy Ahr Richard E. Bingham Patrick S. Broos Mary J. Carter Barry K. Hancock Howard E. Huckle S D. Hunsberger Hajime Kawakami Ronnie Killough T Scott Koch Michael K. Mclelland Kelly Smith Philip J. Smith Juan Carlos Soto Patricia T. Boyd Alice A. Breeveld Stephen T. Holland Mariya Ivanushkina Michael S. Pryzby Martin D. Still Joseph Stock 《Space Science Reviews》2005,120(3-4):95-142
The Ultra-Violet/Optical Telescope (UVOT) is one of three instruments flying aboard the Swift Gamma-ray Observatory. It is designed to capture the early (∼1 min) UV and optical photons from the afterglow of gamma-ray
bursts in the 170–600 nm band as well as long term observations of these afterglows. This is accomplished through the use
of UV and optical broadband filters and grisms. The UVOT has a modified Ritchey–Chrétien design with micro-channel plate intensified
charged-coupled device detectors that record the arrival time of individual photons and provide sub-arcsecond positioning
of sources. We discuss some of the science to be pursued by the UVOT and the overall design of the instrument. 相似文献
998.
北斗导航系统完好性是指北斗导航系统不能用于导航服务或导航精度超出给定范围时,具备及时发现故障并通知用户的能力.针对北斗导航完好性检测问题,为改善北斗导航定位系统的精度、连续性、完好性和可用性,研究了基于惯性辅助的北斗导航故障检测方法,设计了北斗导航系统的量测修正与故障检测实现方案,构建了基于新息正交性的自适应滤波北斗/SINS紧组合导航架构,根据滑动窗口内新息动态变化特性修正系统量测噪声方差,在北斗导航信号受到较大干扰、发生异常的情况下,对品质较差的卫星测量信号进行识别,并对检测超出一定阈值的突变卫星信号实现故障隔离,从而提高系统适应能力,增强北斗/SINS紧组合导航系统容错性.构建了北斗/SINS组合导航系统仿真验证模型,结果表明,基于惯性辅助的北斗导航方法能够有效检测出卫星信号故障,提高了系统的适应性和定位精度. 相似文献
999.
1000.
《中国航空学报》2023,36(5):363-376
Cubature Kalman Filter (CKF) offers a promising solution to handle the data fusion of integrated nonlinear INS/GNSS (Inertial Navigation System/Global Navigation Satellite System) navigation. However, its accuracy is degraded by inaccurate kinematic noise statistics which originate from disturbances of system dynamics. This paper develops a method of closed-loop feedback covariance control to address the above problem of CKF. In this method, the posterior state and its covariance are fed back to the filtering process to constitute a closed-loop structure for CKF covariance propagation. Subsequently, based on the maximum likelihood principle, a control scheme of the prior state covariance is established by using the feedback state and covariance within an estimation window and further adopting a proportional coefficient to amplify the feedback terms in recent time steps for the full use of new information to reflect actual system characteristics. Since it does not directly use kinematic noise covariance, the proposed method can effectively avoid the adverse impact of inaccurate kinematic noise statistics on filtering solutions. Further, it can also guarantee the prior state covariance to be positive semi-definite without involving extra measures. The efficacy of the proposed method is validated by simulations and experiments for integrated INS/GNSS navigation. 相似文献