Next Article in Journal
Aeroacoustic and Aerodynamic Adjoint-Based Shape Optimization of an Axisymmetric Aero-Engine Intake
Next Article in Special Issue
An Improved Multi-Objective Particle Swarm Optimization Method for Rotor Airfoil Design
Previous Article in Journal
Optimal Collaborative Scheduling of Multi-Aircraft Types for Forest Fires General Aviation Rescue
Previous Article in Special Issue
EVTOL Tilt-Wing Aircraft Design under Uncertainty Using a Multidisciplinary Possibilistic Approach
 
 
Article
Peer-Review Record

Research on Pilot Control Strategy and Workload for Tilt-Rotor Aircraft Conversion Procedure

Aerospace 2023, 10(9), 742; https://doi.org/10.3390/aerospace10090742
by Xufei Yan 1, Ye Yuan 2,* and Renliang Chen 3
Reviewer 1: Anonymous
Reviewer 2: Anonymous
Aerospace 2023, 10(9), 742; https://doi.org/10.3390/aerospace10090742
Submission received: 26 June 2023 / Revised: 16 August 2023 / Accepted: 20 August 2023 / Published: 22 August 2023
(This article belongs to the Special Issue E-VTOL Simulation and Autonomous System Development)

Round 1

Reviewer 1 Report

This paper studies the pilot control strategy and workload of tilt-rotor aircraft dynamic conversion procedure between helicopter mode and fixed-wing mode. Based on the nonlinear flight dynamics model, a nonlinear optimal control model of dynamic conversion is constructed, considering factors such as conversion corridor limitations, pilot control, flight attitude, engine rated power, and wing stall effects. To assess pilot workload, an analytical method based on wavelet transform is proposed. In general, this work is of great significance in terms of tilt-rotor aircraft design and operation. I have several main concerns as follows:

1).What the authors are talking about using "nonlinear optimal control model"? Whether or not a real human pilot is in the loop to operate the tilt-rotor aircraft?Or, do you mean: the "nonlinear optimal control model" is a representative of the human pilot?The authors should give the control structure blocks (charts) including the aircraft, control model for the simulation closed-loop model. More details need to be given to make this clear.

2).In the paragraph "Therefore, this paper first employs nonlinear optimal control theory to ...", the innovations are not clear, and need to be reformulated, e.g., what is the difference or the advantages of your methods.

3). what is the application places for the findings (control strategies) in real flight of tilt-rotor aircraft? Is a real human pilot needed or not in future is your control model is adopted in flight control computer?

English writing is good in general, however, in some places grammar should be checked for this paper. 

Author Response

Please see the attachment.

Author Response File: Author Response.pdf

Reviewer 2 Report

Please, check the uploaded file.

Comments for author File: Comments.zip


Author Response

Please see the attachment.

Author Response File: Author Response.pdf

Round 2

Reviewer 1 Report

The author has well replied the reviewer's comments.This paper can be accepted after minor English grammar revisions.

Minor English grammar revisions are still needed. The authors should read through the manuscript, and make possible changes.

Reviewer 2 Report

Thank you for your valuable answers, I have appreciated the effort to answer all the questions related to the manuscript.

 

Back to TopTop