Triple difference-based spacecraft GPS/INS attitude determination

Xiaokui Yue; Jianping Yuan

Triple difference-based spacecraft GPS/INS attitude determination

Xiaokui Yue, Jianping Yuan

School of Astronautics

Northwestern Polytechnical University Xian

Research output: Contribution to journal › Article › peer-review

1 Scopus citations

Abstract

Based on the triple difference carrier phase observables, a GPS/INS integration algorithm for attitude determination is studied. The proposed integration system also contains a cycle slip detection algorithm, in which inertial information is utilized to detect cycle slip. Some computer simulations are performed to verify the proposed integration system. The results show that accurate and reliable navigation solution can be gained.

Original language	English
Pages (from-to)	1-5+10
Journal	Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology
Volume	26
Issue number	4
State	Published - Aug 2006

Keywords

Carrier phase
Combinatorial algorithm
Global positioning system
Inertial measurement
Simulation
Spacecraft

Cite this

@article{d7c96bcb04f14a83b263ec1cfda9c7d2,

title = "Triple difference-based spacecraft GPS/INS attitude determination",

abstract = "Based on the triple difference carrier phase observables, a GPS/INS integration algorithm for attitude determination is studied. The proposed integration system also contains a cycle slip detection algorithm, in which inertial information is utilized to detect cycle slip. Some computer simulations are performed to verify the proposed integration system. The results show that accurate and reliable navigation solution can be gained.",

keywords = "Carrier phase, Combinatorial algorithm, Global positioning system, Inertial measurement, Simulation, Spacecraft",

author = "Xiaokui Yue and Jianping Yuan",

year = "2006",

month = aug,

language = "英语",

volume = "26",

pages = "1--5+10",

journal = "Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology",

issn = "1000-758X",

publisher = "Chinese Academy of Space Technology",

number = "4",

}

TY - JOUR

T1 - Triple difference-based spacecraft GPS/INS attitude determination

AU - Yue, Xiaokui

AU - Yuan, Jianping

PY - 2006/8

Y1 - 2006/8

N2 - Based on the triple difference carrier phase observables, a GPS/INS integration algorithm for attitude determination is studied. The proposed integration system also contains a cycle slip detection algorithm, in which inertial information is utilized to detect cycle slip. Some computer simulations are performed to verify the proposed integration system. The results show that accurate and reliable navigation solution can be gained.

AB - Based on the triple difference carrier phase observables, a GPS/INS integration algorithm for attitude determination is studied. The proposed integration system also contains a cycle slip detection algorithm, in which inertial information is utilized to detect cycle slip. Some computer simulations are performed to verify the proposed integration system. The results show that accurate and reliable navigation solution can be gained.

KW - Carrier phase

KW - Combinatorial algorithm

KW - Global positioning system

KW - Inertial measurement

KW - Simulation

KW - Spacecraft

UR - http://www.scopus.com/inward/record.url?scp=33750323526&partnerID=8YFLogxK

M3 - 文章

AN - SCOPUS:33750323526

SN - 1000-758X

VL - 26

SP - 1-5+10

JO - Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology

JF - Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology

IS - 4

ER -

Triple difference-based spacecraft GPS/INS attitude determination

Abstract

Keywords

Other files and links

Fingerprint

Cite this