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

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

Type: Journal

Type of Copyright:

Languages: English

Open Access Policy:

Type of publications:

Publication frecuency: -

Categories: Aerospace Engineering (Q1) Applied Mathematics (Q1) Control and Systems Engineering (Q1) Electrical and Electronic Engineering (Q1) Space and Planetary Science (Q1)

Price

- €

Inmediate OA

NPD

Embargoed OA

- €

Non OA

Metrics

Journal of Guidance, Control, and Dynamics

1,573

SJR Impact factor

143

H Index

223

Total Docs (Last Year)

729

Total Docs (3 years)

6675

Total Refs

2494

Total Cites (3 years)

717

Citable Docs (3 years)

3,18

Cites/Doc (2 years)

29,93

Ref/Doc

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Astrophysical Journal Letters Q1
Astrophysical Journal, Supplement Series Q1
Earth and Planetary Science Letters Q1
Astronomical Journal Q1

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Aims and Scope

Best articles by citations

Canonical Solution of Two-Point Boundary-Value Problems

Kalman Filtering for Spacecraft System Alignment Calibration

Precise Cassini Navigation During Solar Conjunctions Through Multifrequency Plasma Calibrations

Generic Smoothing for Optimal Bang-Off-Bang Spacecraft Maneuvers

State-Space Interpolation for a Gain-Scheduled Autopilot

Optimization of Variable-Specific-Impulse Interplanetary Trajectories

Optimal Control Problem for Low-Thrust Multiple Asteroid Tour Missions

Double-Homotopy Method for Solving Optimal Control Problems

Robust Linear Output Feedback Control of an Airbreathing Hypersonic Vehicle

Fast Homotopy Method for Asteroid Landing Trajectory Optimization Using Approximate Initial Costates

Numerical Time-Scale Separation for Rotorcraft Nonlinear Optimal Control Analyses

Stability Limits of Spinning Missiles with Attitude Autopilot

SHOW MORE ARTICLES

Unified Approach to Modeling and Control of Rigid Multibody Systems

In-Flight Trajectory Planning and Guidance for Autonomous Parafoils

Infinite-Horizon Control for Retrieving a Tethered Subsatellite via an Elastic Tether

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

Identification of Multimodal Pilot Models Using Ramp Target and Multisine Disturbance Signals

Incremental Approximate Dynamic Programming for Nonlinear Adaptive Tracking Control with Partial Observability

Feedback Guidance in Uncertain Spatiotemporal Wind Using a Vector Backstepping Algorithm

Susceptibility of F/A-18 Flight Controllers to the Falling-Leaf Mode: Linear Analysis

Optimal Angular Velocity Estimation of Spacecraft Using only Star Tracker Measurements

Nonlinear H8 Attitude Control Using Modified Rodrigues Parameters

Erratum: Gust Energy Extraction for Mini and Micro Uninhabited Aerial Vehicles

Equivalency Between Strapdown Inertial Navigation Coning and Sculling Integrals/Algorithms

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