Default: Journal of Guidance, Control, and Dynamics

ISSN: 0731-5090

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Journal of Guidance, Control, and Dynamics Q1 Unclaimed

American Institute of Aeronautics and Astronautics Inc. (AIAA) United States
Unfortunately this journal has not been claimed yet. For this reason, some information may be unavailable.

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 135. It has an SJR impact factor of 1,573 and it has a best quartile of Q1. It is published in English.

Type: Journal

Type of Copyright:

Languages: English

Open Access Policy:

Type of publications:

Publication frecuency: -

Metrics

Journal of Guidance, Control, and Dynamics

1,573

SJR Impact factor

135

H Index

184

Total Docs (Last Year)

803

Total Docs (3 years)

5720

Total Refs

2938

Total Cites (3 years)

787

Citable Docs (3 years)

3,4

Cites/Doc (2 years)

31,09

Ref/Doc


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A Unified Mathematical Framework for Strapdown Algorithm Design

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Absolute Orbit and Gravity Determination Using Relative Position Measurements Between Two Satellites

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Adaptive Glide Slope Control for Parafoil and Payload Aircraft

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Adaptive Loop Transfer Recovery

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Adaptive Model Inversion Flight Control for Tilt-Rotor Aircraft

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Adaptively Robust Unscented Kalman Filter for Tracking a Maneuvering Vehicle

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All-Electric Spacecraft Precision Pointing Using Model Predictive Control

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Alternating Orbiter Strategy for Asteroid Exploration

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Analytical Expressions that Characterize Propellantless Capture with Electrostatically Charged Spacecraft

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

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Annual Business and News: Beginning the 34th Year

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Aspects of Control for a Parafoil and Payload System

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Asymptotic Tracking Control for Spacecraft Formation Flying with Decentralized Collision Avoidance

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Attitude Dynamics of the Classical Dumbbell Problem with Solar Radiation Pressure

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Attitude Propagation for a Slewing Angular Rate Vector

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Automated Generation of Symmetric Lunar Free-Return Trajectories

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Autonomous Trajectory Planning for Rendezvous and Proximity Operations by Conic Optimization

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Avoiding Lockout Instability for Towed Parafoil Systems

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Canonical Solution of Two-Point Boundary-Value Problems

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Comparison of Adaptive Control Architectures for Flutter Suppression

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Compressed polynomial approach for onboard ephemeris representation

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

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Continuous-Time Kalman Filtering with Implicit Discrete Measurement Times

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