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verified SJR 1,218 · Q1 • database Scopus / SJR & Web of Science indexed
Journal of Guidance, Control, and Dynamics
United States · American Institute of Aerona...
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Journal of Guidance, Control, and Dynamics

Journal of Guidance, Control, and Dynamics is a journal indexed in SJR in Space and Planetary Science and Electrical and Electronic Engineering with an H index of 170. It has an SJR impact factor of 1,218 and it has a best quartile of Q1. It is published in English. It has an SJR impact factor of 1,218.

ISSN: 0731-5090
Publisher: American Institute of Aeronautics and Astronautics Inc. (AIAA)
Category: Space and Planetary Science
Indexation: verifiedScopus / SJR verifiedWeb of Science
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schedule CountryOfPapers database fields
SJR Impact Factor trending_up
1,218 Q1
H-index 170
Acceptance rate pie_chart
21% Selective
Source Acceptance_Rate
Time to publication hourglass_top
NPD
Field NPD
Publication cost (APC) payments
NPD Subscription
Non-OA path NPD

Metrics

Scimago and CountryOfPapers database fields

Scopus / SJR Web of Science

SJR Impact

1,218

H-index

170

Docs (year)

210

Docs 3y

583

Total refs

7577

Cites 3y

2219

Citable 3y

424

Cites/Doc 2y

3.49

Ref/Doc

36.08

Immediate OA

—

Embargoed OA

NPD

Non OA / Submission

—

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Best articles by citations

Aspects of Control for a Parafoil and Payload System

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Wind Uncertainty Modeling and Robust Trajectory Planning for Autonomous Parafoils

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Continuous-Time Kalman Filtering with Implicit Discrete Measurement Times

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Conflict-Free Trajectory Planning Based on a Data-Driven Conflict-Resolution Model

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Compressed polynomial approach for onboard ephemeris representation

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Comparison of Adaptive Control Architectures for Flutter Suppression

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Canonical Solution of Two-Point Boundary-Value Problems

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Avoiding Lockout Instability for Towed Parafoil Systems

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Autonomous Trajectory Planning for Rendezvous and Proximity Operations by Conic Optimization

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Automated Generation of Symmetric Lunar Free-Return Trajectories

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Attitude Propagation for a Slewing Angular Rate Vector

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Attitude Dynamics of the Classical Dumbbell Problem with Solar Radiation Pressure

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Angular-Momentum Management of Spacecraft Electromagnetic Docking Considering the Earth's Magnetic Field

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Alternating Orbiter Strategy for Asteroid Exploration

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Adaptively Robust Unscented Kalman Filter for Tracking a Maneuvering Vehicle

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