Asteroid Approaching Orbit Optimization Considering Optical Navigation Observability-Reference-Cited by-同舟云学术

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Asteroid Approaching Orbit Optimization Considering Optical Navigation Observability

Published:2022-12 Issue:6 Volume:58 Page:5165-5179
ISSN:0018-9251
Container-title:IEEE Transactions on Aerospace and Electronic Systems
language:
Short-container-title:IEEE Trans. Aerosp. Electron. Syst.

Author:

Qiao Dong¹^ORCID,Zhou Xingyu²^ORCID,Zhao Zeduan³,Qin Tong⁴^ORCID

Affiliation:

1. State Key Laboratory of Astronautic Dynamics, School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China

2. School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China

3. Nanjing Research Institute of Electronic Engineering, Nanjing, China

4. School of Information and Electronics, Beijing Institute of Technology, Beijing, China

Funder

National Natural Science Foundation of China

National Defense Basic Scientific Research Project

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Aerospace Engineering

Link

http://xplorestaging.ieee.org/ielx7/7/9970423/09757848.pdf?arnumber=9757848

Reference46 articles.

1. On the Fisher Information Matrix for Multivariate Elliptically Contoured Distributions

2. Observability and fisher information matrix in nonlinear regression

3. Model Predictive Control of Swarms of Spacecraft Using Sequential Convex Programming

4. Solving Nonconvex Optimal Control Problems by Convex Optimization

5. Modified Genetic Algorithm for Constrained Trajectory Optimization

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