2018 AIAA Atmospheric Flight Mechanics Conference
Latest Publications

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(FIVE YEARS 0)

H-INDEX

(FIVE YEARS 0)

Published By American Institute Of Aeronautics And Astronautics

9781624105258

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

Correction: Near-Optimal Entry Guidance for Reference Trajectory Tracking via Convex Optimization

2018 AIAA Atmospheric Flight Mechanics Conference ◽

10.2514/6.2018-0013.c1 ◽

2018 ◽

Author(s):

Zhenbo Wang ◽

Michael J. Grant

Keyword(s):

Convex Optimization ◽

Trajectory Tracking ◽

Reference Trajectory ◽

Entry Guidance

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Correction: Path Constraint Regularization in Optimal Control Problems using Saturation Functions

2018 AIAA Atmospheric Flight Mechanics Conference ◽

10.2514/6.2018-0018.c1 ◽

2018 ◽

Author(s):

Thomas Antony ◽

Michael J. Grant

Keyword(s):

Optimal Control ◽

Optimal Control Problems ◽

Control Problems ◽

Path Constraint

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Correction: The Relaxed Autonomously Switched Hybrid System (RASHS) Approach to Indirect Multi-Phase Trajectory Optimization for Aerospace Vehicles

2018 AIAA Atmospheric Flight Mechanics Conference ◽

10.2514/6.2018-0016.c1 ◽

2018 ◽

Cited By ~ 1

Author(s):

Harish Saranathan ◽

Michael J. Grant

Keyword(s):

Hybrid System ◽

Phase Trajectory ◽

Trajectory Optimization ◽

Aerospace Vehicles ◽

Multi Phase

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Mars Helicopter Technology Demonstrator

2018 AIAA Atmospheric Flight Mechanics Conference ◽

10.2514/6.2018-0023 ◽

2018 ◽

Cited By ~ 35

Author(s):

Bob Balaram ◽

Timothy Canham ◽

Courtney Duncan ◽

Håvard F. Grip ◽

Wayne Johnson ◽

...

Keyword(s):

Technology Demonstrator

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Fly-by-Feel Control of an Aeroelastic Aircraft using Distributed Multi-Rate Kalman Filtering

2018 AIAA Atmospheric Flight Mechanics Conference ◽

10.2514/6.2018-1012 ◽

2018 ◽

Author(s):

George J. Armanious ◽

Richard C. Lind

Keyword(s):

Kalman Filtering

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Evaluation of Aeroelastic Effects on Pilot-Induced Oscillations via Pilot-in-the-Loop Simulations

2018 AIAA Atmospheric Flight Mechanics Conference ◽

10.2514/6.2018-1016 ◽

2018 ◽

Cited By ~ 1

Author(s):

Daniel Drewiacki ◽

Flavio J. Silvestre ◽

Antonio Bernardo Guimaraes Neto

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High Angle of Attack Static and Dynamic Modeling Methods for Flight Dynamics Loss of Control Research

2018 AIAA Atmospheric Flight Mechanics Conference ◽

10.2514/6.2018-1021 ◽

2018 ◽

Cited By ~ 1

Author(s):

David C. Hyde ◽

Frank Brown ◽

Kamal M. Shweyk ◽

Kevin Cunningham ◽

Gautam H. Shah

Keyword(s):

Dynamic Modeling ◽

Angle Of Attack ◽

Flight Dynamics ◽

Loss Of Control ◽

High Angle ◽

High Angle Of Attack ◽

Modeling Methods ◽

Control Research

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Studying the Effect of the Tail on the Dynamics of a Flapping-Wing MAV using Free-Flight Data

2018 AIAA Atmospheric Flight Mechanics Conference ◽

10.2514/6.2018-0524 ◽

2018 ◽

Cited By ~ 1

Author(s):

Frank G. Rijks ◽

Matej Karásek ◽

Sophie F. Armanini ◽

Coen C. de Visser

Keyword(s):

Flapping Wing ◽

Free Flight ◽

Flight Data

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Linking the Pilot Structural Model and Pilot Workload

2018 AIAA Atmospheric Flight Mechanics Conference ◽

10.2514/6.2018-0533 ◽

2018 ◽

Author(s):

Edward N. Bachelder ◽

Ronald A. Hess ◽

Martine Godfroy-Cooper ◽

Bimal L. Aponso

Keyword(s):

Structural Model

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High Angle of Attack Aerodynamic Model Identification for Spin Recovery Simulation Using Non-Parametric Smoothing Functions

2018 AIAA Atmospheric Flight Mechanics Conference ◽

10.2514/6.2018-0772 ◽

2018 ◽

Cited By ~ 2

Author(s):

Roberto Bunge ◽

Ilan Kroo

Keyword(s):

Angle Of Attack ◽

Model Identification ◽

High Angle ◽

High Angle Of Attack ◽

Aerodynamic Model ◽

Smoothing Functions ◽

Recovery Simulation ◽

Non Parametric

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2018 AIAA Atmospheric Flight Mechanics ConferenceLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By American Institute Of Aeronautics And Astronautics

Correction: Near-Optimal Entry Guidance for Reference Trajectory Tracking via Convex Optimization

Correction: Path Constraint Regularization in Optimal Control Problems using Saturation Functions

Correction: The Relaxed Autonomously Switched Hybrid System (RASHS) Approach to Indirect Multi-Phase Trajectory Optimization for Aerospace Vehicles

Mars Helicopter Technology Demonstrator

Fly-by-Feel Control of an Aeroelastic Aircraft using Distributed Multi-Rate Kalman Filtering

Evaluation of Aeroelastic Effects on Pilot-Induced Oscillations via Pilot-in-the-Loop Simulations

High Angle of Attack Static and Dynamic Modeling Methods for Flight Dynamics Loss of Control Research

Studying the Effect of the Tail on the Dynamics of a Flapping-Wing MAV using Free-Flight Data

Linking the Pilot Structural Model and Pilot Workload

High Angle of Attack Aerodynamic Model Identification for Spin Recovery Simulation Using Non-Parametric Smoothing Functions

2018 AIAA Atmospheric Flight Mechanics Conference
Latest Publications