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Aircraft Characterization in Icing Using Flight Test Data
- E. Whalen and
- M. B. Bragg
May-Jun. 2005Journal of Aircraft Volume 42, Issue 3
https://doi.org/10.2514/1.11198
- First Page
- Read Now
No Access
Morphing Wing Flight Control Via Postbuckled Precompressed Piezoelectric Actuators
- Roelof Vos ,
- Roeland De Breuker ,
- Ron Barrett and
- Paolo Tiso
Jul/Aug 2007Journal of Aircraft Volume 44, Issue 4
https://doi.org/10.2514/1.21292
- First Page
- Read Now
No Access
Feasible Trajectory Generation for Atmospheric Entry Guidance
- James A. Leavitt and
- Kenneth D. Mease
Mar./Apr 2007Journal of Guidance, Control, and Dynamics Volume 30, Issue 2
https://doi.org/10.2514/1.23034
- First Page
- Read Now
No Access
Neural-Network-Based Design of Optimal Controllers for Nonlinear Systems
- Nilesh V. Kulkarni and
- Minh Q. Phan
Sep./Oct. 2004Journal of Guidance, Control, and Dynamics Volume 27, Issue 5
https://doi.org/10.2514/1.2320
- First Page
- Read Now
No Access
Retrofit Fault-Tolerant Flight Control Design Under Control Effector Damage
- Jovan D. Boskovic ,
- Ravi Prasanth and
- Raman K. Mehra
May/June 2007Journal of Guidance, Control, and Dynamics Volume 30, Issue 3
https://doi.org/10.2514/1.25564
- First Page
- Read Now
No Access
Rate-Based Model Predictive Control of Turbofan Engine Clearance
- Jonathan A. DeCastro
July/Aug. 2007Journal of Propulsion and Power Volume 23, Issue 4
https://doi.org/10.2514/1.25846
- First Page
- Read Now
No Access
System Identification for Retrofit Reconfigurable Control of an F/A-18 Aircraft
- David G. Ward and
- Jeffrey F. Monaco
Jan./Feb. 2005Journal of Aircraft Volume 42, Issue 1
https://doi.org/10.2514/1.2941
- First Page
- Read Now
No Access
Design of Static H8 Linear Parameter Varying Controllers for Unmanned Aircraft
- Kannan Natesan ,
- Da-Wei Gu and
- Ian Postlethwaite
Nov./Dec. 2007Journal of Guidance, Control, and Dynamics Volume 30, Issue 6
https://doi.org/10.2514/1.31283
- First Page
- Read Now
No Access
Trajectory-Shaping Guidance for Interception of Ballistic Missiles During the Boost Phase
- John A. Lukacs IV and
- Oleg A. Yakimenko
Sept/Oct. 2008Journal of Guidance, Control, and Dynamics Volume 31, Issue 5
https://doi.org/10.2514/1.32262
- First Page
- Read Now
No Access
Optimum Design of a Compound Helicopter
- Hyeonsoo Yeo and
- Wayne Johnson
July/Aug. 2009Journal of Aircraft Volume 46, Issue 4
https://doi.org/10.2514/1.40101
- First Page
- Read Now
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Application of Design of Experiments to Flight Test: A Case Study
- Aaron A. Tucker ,
- Gregory T. Hutto and
- Cihan H. Dagli
Mar./Apr. 2010Journal of Aircraft Volume 47, Issue 2
https://doi.org/10.2514/1.40301
- First Page
- Read Now
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Dynamic Sensitivity to Atmospheric Turbulence of Unmanned Air Vehicles with Varying Configuration
- Mujahid Abdulrahim ,
- Simon Watkins ,
- Reuven Segal ,
- Matthew Marino and
- John Sheridan
Nov./Dec. 2010Journal of Aircraft Volume 47, Issue 6
https://doi.org/10.2514/1.46860
- First Page
- Read Now
No Access
Implementation of a Flapping Wing Micro Air Vehicle Control Technique
- Michael L. Anderson and
- Richard G. Cobb
27 December 2013Journal of Guidance, Control, and Dynamics Volume 37, Issue 1
https://doi.org/10.2514/1.57855
Abstract
Abstract
Flapping wing micro air vehicles continue to be a growing field, with ongoing research into unsteady, low Reynolds number aerodynamics, microfabrication, and fluid–structure interaction. However, research into flapping wing control of such micro air ...
No Access
Classical and Simple Adaptive Control for Nonminimum Phase Autopilot Design
- Itzhak Barkana
July/Augu 2005Journal of Guidance, Control, and Dynamics Volume 28, Issue 4
https://doi.org/10.2514/1.9542
- First Page
- Read Now
No Access
Method for Determination of Nonlinear Attainable Moment Sets
- Michael A. Bolender and
- David B. Doman
Sep./Oct. 2004Journal of Guidance, Control, and Dynamics Volume 27, Issue 5
https://doi.org/10.2514/1.9548
- First Page
- Read Now
No Access
Transient Poststall Aerodynamic Modeling for Extreme Maneuvers in Micro Air Vehicles
Mar./Apr. 2011Journal of Aircraft Volume 48, Issue 2
https://doi.org/10.2514/1.C000278
- First Page
- Read Now
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Analytical Criterion for Aircraft Spin Susceptibility
- A. A. Paranjape and
- N. Ananthkrishnan
Sept./Oct 2010Journal of Aircraft Volume 47, Issue 5
https://doi.org/10.2514/1.C031010
- First Page
- Read Now
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Alternative Trim Analysis Formulations for Vehicles with Redundant Multi-Axis Control Surfaces
- Daniel C. Garmendia and
- Dimitri N. Mavris
24 April 2015Journal of Aircraft Volume 53, Issue 1
https://doi.org/10.2514/1.C033184
Abstract
Abstract
Conventional trim optimization problem formulations can produce poor results for vehicles with redundant multi-axis control surfaces. Trimming these vehicles requires solving the nonlinear equations of motion for their roots or equilibrium points. The ...
Free Access
Simulation Study of Severity and Mitigation of Wake-Vortex Encounters in Ground Proximity
10 May 2017Journal of Aircraft Volume 54, Issue 5
https://doi.org/10.2514/1.C033995
Abstract
Abstract
Wake-vortex encounter reports as well as simulations show a significantly higher encounter probability during landing shortly before touchdown in comparison to other flight phases. This is caused, among other factors, by the special behavior of wake ...
No Access
How Plate Lines Influence the Hazard Perception of Pilots During Wake Encounters
15 December 2019Journal of Aircraft Volume 57, Issue 2
https://doi.org/10.2514/1.C035689
Abstract
Abstract
In free air aircraft, wake vortices descend due to their mutually induced velocities. In ground proximity, however, they are hindered to descent, which increases the encounter risk significantly. Recent investigations showed that vortex decay in ground ...

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Aircraft Characterization in Icing Using Flight Test Data

Morphing Wing Flight Control Via Postbuckled Precompressed Piezoelectric Actuators

Feasible Trajectory Generation for Atmospheric Entry Guidance

Neural-Network-Based Design of Optimal Controllers for Nonlinear Systems

Retrofit Fault-Tolerant Flight Control Design Under Control Effector Damage

Rate-Based Model Predictive Control of Turbofan Engine Clearance

System Identification for Retrofit Reconfigurable Control of an F/A-18 Aircraft

Design of Static H8 Linear Parameter Varying Controllers for Unmanned Aircraft

Trajectory-Shaping Guidance for Interception of Ballistic Missiles During the Boost Phase

Optimum Design of a Compound Helicopter

Application of Design of Experiments to Flight Test: A Case Study

Dynamic Sensitivity to Atmospheric Turbulence of Unmanned Air Vehicles with Varying Configuration

Implementation of a Flapping Wing Micro Air Vehicle Control Technique

Abstract

Classical and Simple Adaptive Control for Nonminimum Phase Autopilot Design

Method for Determination of Nonlinear Attainable Moment Sets

Transient Poststall Aerodynamic Modeling for Extreme Maneuvers in Micro Air Vehicles

Analytical Criterion for Aircraft Spin Susceptibility

Alternative Trim Analysis Formulations for Vehicles with Redundant Multi-Axis Control Surfaces

Abstract

Simulation Study of Severity and Mitigation of Wake-Vortex Encounters in Ground Proximity

Abstract

How Plate Lines Influence the Hazard Perception of Pilots During Wake Encounters

Abstract