Pulsar/Star Tracker/INS Integrated Navigation Method Based on Asynchronous Observation Model-Reference-Cited by-同舟云学术

Pulsar/Star Tracker/INS Integrated Navigation Method Based on Asynchronous Observation Model

Published:2019-09 Issue:5 Volume:32 Page:04019075
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Sun Jian¹,Guo Pengbin²,Wu Teng³,Chen Gang⁴

Affiliation:

1. Associate Professor, State Key Laboratory for Strength and Vibration, Shaanxi Engineering Laboratory for Vibration Control of Aerospace Structures, School of Aerospace, Xi’an Jiaotong Univ., Xi’an 710049, PR China.

2. Assistant Researcher, Key Laboratory of Space Utilization, Technology, and Engineering Center for Space Utilization, Chinese Academy of Sciences, Beijing 100094, PR China.

3. Ph.D. Student, State Key Laboratory for Strength and Vibration, Shaanxi Engineering Laboratory for Vibration Control of Aerospace Structures, School of Aerospace, Xi’an Jiaotong Univ., Xi’an 710049, PR China.

4. Professor, State Key Laboratory for Strength and Vibration, Shaanxi Engineering Laboratory for Vibration Control of Aerospace Structures, School of Aerospace, Xi’an Jiaotong Univ., Xi’an 710049, PR China (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001045

Reference14 articles.

1. Interplanetary spacecraft navigation using pulsars

2. X-Ray Pulsar-Based Relative Navigation using Epoch Folding

3. Autonomous orbit determination and its error analysis for deep space using X-ray pulsar

4. Multi-sensor optimal data fusion for INS/GPS/SAR integrated navigation system

5. Multirate Observation-Based X-Ray Pulsar Navigation Technique

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