检索结果-内蒙古大学图书馆

Survey of Global-Positioning-System-Based attitude determination algorithms

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 2017年第6期40卷 1321-1335页

作者： Goh, Shu Ting Low, Kay-Soon Nanyang Technol Univ Satellite Res Ctr Sch Elect & Elect Engn S2-2-B3-0650 Singapore 639798 Singapore Natl Univ Singapore Dept Elect & Comp Engn E4 04-17 Singapore 117583 Singapore

The phase quartic algorithm and attitude-lean-loping estimator with GPS recursive operations (ALLEGRO) have been proposed in a study. Both of these algorithms demonstrate a high rate of error convergence. The phase quartic is an eigenvalue-based estimation algorithm, whereas ALLEGRO is derived based on the minimal model error estimation algorithm. The quaternion vector has been used as the primary attitude representation, except for direction computational matrix (DCM) and attitude matrix solution (AMES) methods. The DCM uses Euler angles, whereas AMES uses nine elements of the attitude matrix as the attitude representation. This study focuses mainly on the existing real-time GPS-based attitude determination methods that are feasible for space application.

关键词： GPS attitude determination algorithms Unscented Kalman Filter Low Earth Orbit Satellites Satellite Navigation American Astronautical Society GPS Receivers Singular Value Decomposition Navigation Satellites Body Reference Frame

来源：评论

学校读者我要写书评

暂无评论

Generalized attitude determination with One Dominant Vector Observation

引用

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 2019年第4期42卷 885-893页

作者： Crassidis, John L. Cheng, Yang Univ Buffalo State Univ New York Dept Mech & Aerosp Engn Amherst NY 14260 USA Mississippi State Univ Dept Aerosp Engn Mississippi State MS 39762 USA

来源：评论

学校读者我要写书评

暂无评论

Spin-Axis attitude determination and Covariances in Local Sun-Earth Frame

引用

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 2011年第6期34卷 1720-1727页

作者： van der Ha, Jozef C. Mission Design & Operat Deming WA 98244 USA

This paper presents practical analytical models for spin-axis attitude determination using measurements generated by sun and Earth sensors. In particular, explicit expressions for the least-squares estimates and their associated covariance matrices are established. The adoption of the local reference frame defined by the instantaneous sun and Earth vectors leads to compact analytical results. These results provide a more immediate understanding of the attitude error covariance matrix in terms of its dependence on the sun Earth geometry. The application of the covariance results is illustrated by using the actual geometrical in-orbit conditions of two satellites.

关键词： Earth Earth Sensors Geostationary Satellites Orbital Period Geostationary Transfer Orbit Bipropellants Extended Kalman Filter Earth Reference Frame Solid Rocket Motor attitude determination algorithms

来源：评论

学校读者我要写书评

暂无评论

Equal-chord attitude determination method for spinning spacecraft

引用

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 2005年第5期28卷 997-1005页

作者： van der Ha, JC Space Design & Operat Columbia MD 21044 USA

The equal-chord method offers a straightforward and low-cost technique for the determination of the spin-axis attitude using sun and Earth sensor data. The Earth aspect angle follows from the time at which the chord lengths measured by the Earth sensor's two pencil beams are equal. An estimation technique is not required, but linear or quadratic fitting of the sensor data should be performed to remove the random errors. The accuracy of the attitude solution obtained by the equal-chord method in the presence of the relevant biases is evaluated. The result is insensitive to uniform biases in-the measured chord angles, caused for instance by errors in the Earth's infrared horizon. Finally, the application of the method is demonstrated using actual flight data of the CONTOUR spacecraft.

关键词： Spinning Spacecraft Earth Sensors Earth Sensors Flight Data Geostationary Transfer Orbit Perigee Kalman Filter Telemetry attitude determination algorithms

来源：评论

学校读者我要写书评

暂无评论

attitude determination IN HIGHER DIMENSIONS

引用

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 1993年第2期16卷 393-395页

作者： SHUSTER, MD Johns Hopkins University Applied Physics Laboratory Laurel Maryland 20723

Generally, one has little cause to estimate an attitude in spaces of dimension higher than three. This exercise, however, affords an insight into the workings of a well-known attitude determination algorithm in three dimensions. In addition, should the dimensionality of our world ever increase without notice, we will be all the better prepared.

关键词： Triad Method Propellant Earth attitude determination algorithms Numerical Integration Space Navigation Optimal Control Canonical Units

来源：评论

学校读者我要写书评

暂无评论

Global positioning system-based attitude determination and the orthogonal procrustes problem

引用

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 2003年第5期26卷 820-822页

作者： Bell, T Lockheed Martin Management & Data Syst Metr Anal Philadelphia PA 19101 USA

The determination of attitude from differential GPS range measurements was posed as an orthogonal Procrustes problem so that a closed-form solution could be found. It was shown that the attitude determination problem could be solved in not one but two different methods. The first method allowed for coplanar baselines, whereas the second method allowed for planar satellite geometry. Subsequent sensitivity and covariance analysis showed that both solutions yielded unbiased estimates. For small attitude changes, a general expression was derived for the covariance of the attitude solution that showed how poor geometry could adversely affect solution quality. (CSA)

关键词： GPS Satellites Singular Value Decomposition GPS Satellites Computing attitude determination algorithms Optimal Control Theory Mathematical Models Sensitivity Analysis Antenna Arrays

来源：评论

学校读者我要写书评

暂无评论

REQUEST: A recursive QUEST algorithm for sequential attitude determination

引用

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 1996年第5期19卷 1034-1038页

作者： BarItzhack, IY NASA GODDARD SPACE FLIGHT CTRFLIGHT MECH BRANCHGREENBELTMD 20771

QUEST is a well-known algorithm for least squares fitting of the attitude quaternion of a spacecraft to vector measurements. QUEST, however, is a single time point (single frame) batch algorithm;thus, measurements that were taken at previous time points are discarded, The algorithm presented provides a recursive routine, which considers all past measurements. The algorithm is based on the fact that the so-called K matrix, one of whose eigenvectors is the sought quaternion, is linearly related to the measured vector pairs and on the ability to propagate K, The extraction of the appropriate eigenvector is done according to the classical QUEST algorithm, This stage, however, can be eliminated, and the computation simplified, if a standard eigenvalue-eigenvector solver algorithm is used.

关键词： Quaternions Extended Kalman Filter Recursive Algorithm attitude determination algorithms Aerospace Engineering Lagrange Multipliers Cartesian Coordinate System Flight Mechanics Control Theory Computing

来源：评论

学校读者我要写书评

暂无评论

attitude determination from Ellipsoid Observations: A Modified Orthogonal Procrustes Problem

引用

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 2018年第10期41卷 2320-2325页

作者： Modenini, D. Univ Bologna Dept Ind Engn DIN Via Fontanelle 40 I-47121 Forli Italy

来源：评论

学校读者我要写书评

暂无评论

Spin-Axis attitude determination Using In-Flight Data

引用

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 2010年第3期33卷 768-781页

作者： van der Ha, Jozef C. Kyushu Univ Dept Aeronaut & Astronaut Fukuoka 8190395 Japan

The paper presents a practical spin-axis attitude determination approach based on the Tanygin-Shuster algorithm. The technique is illustrated by means of sensor measurement data originating from two satellites with very different orbit and attitude characteristics. The most appropriate data intervals are identified using criteria based on measurement sensitivities. A minimum-variance technique is formulated for establishing the Earth aspect angle from the measured chord angles. The chain of covariance transformations from the fundamental sensor measurement errors to the final attitude error is presented. The unit-vector normalization technique, which is an inherent part of the Tanygin-Shuster method, is found to be beneficial for the stability of the attitude determination results under unknown biases, especially in cases in which only a subset of the measurement angles are available.

关键词： Earth Photodetector Meteorological Satellites Flight Data attitude Control Orbital Period attitude determination algorithms Extended Kalman Filter Orbit determination Propellant

来源：评论

学校读者我要写书评

暂无评论

Magnetometer-Only attitude determination Using Novel Two-Step Kalman Filter Approach

引用

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 2012年第6期35卷 1693-1701页

作者： Searcy, Jason D. Pernicka, Henry J. Missouri Univ Sci & Technol Rolla MO 65409 USA

Determining spacecraft attitude in real time using only magnetometer data presents a challenging filtering problem. A flexible and computationally efficient method for solving the spacecraft attitude using only an inexpensive and reliable magnetometer would be a useful option for satellite missions, particularly those with modest budgets. The primary challenge is that magnetometers only instantaneously resolve two axes of the spacecraft attitude. Typically, magnetometers are used in conjunction with other sensors to resolve all three axes. However, by using a filter over an adequately long orbit arc, the magnetometer data can yield full attitude, and in real time. The method presented solves the problem using a two-step extended Kalman filter. In the first step, the magnetic field data are filtered to obtain the magnetic field derivative vector, which is combined with the magnetic field vector in the second step to fully resolve the attitude. A baseline scenario is developed, and a parametric study is conducted using the parameters of interest.

关键词： Unscented Kalman Filter Magnetometers Quaternions Spacecraft attitude Equatorial Orbit Satellites attitude determination algorithms Earth Centered Inertial Polar Orbit Earth's Magnetic Field

来源：评论

学校读者我要写书评

暂无评论

建议与咨询留下您的常用邮箱和电话号码，以便我们向您反馈解决方案和替代方法

时间限定

文献类型

馆藏选择

核心期刊

语言

文献类型

帮助

文字说明：

检索规则说明：

检索范例：

分类表

所选分类

限定检索结果

文献类型

馆藏范围

日期分布

学科分类号

主题

机构

作者

语言

请选择保存的检索档案：

请选择收藏分类：

通借通还

建议与咨询 留下您的常用邮箱和电话号码，以便我们向您反馈解决方案和替代方法

时间限定

文献类型

馆藏选择

核心期刊

语言

文献类型

帮助

文字说明：

检索规则说明：

检索范例：

分类表

所选分类

限定检索结果

文献类型

馆藏范围

日期分布

学科分类号

主题

机构

作者

语言

请选择保存的检索档案： 新增检索档案 确定 取消

请选择收藏分类： 新增自定义分类 确定 取消

通借通还

建议与咨询留下您的常用邮箱和电话号码，以便我们向您反馈解决方案和替代方法

请选择保存的检索档案：

请选择收藏分类：