Flight Envelope Prediction via Optimal Control-Based Reachability Analysis-Reference-Cited by-同舟云学术

Flight Envelope Prediction via Optimal Control-Based Reachability Analysis

Published:2022-01 Issue:1 Volume:45 Page:185-195
ISSN:1533-3884
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Lu Zhidong¹^ORCID,Hong Haichao¹^ORCID,Gerdts Matthias²^ORCID,Holzapfel Florian¹^ORCID

Affiliation:

1. Technical University of Munich, 85748 Garching, Germany

2. Bundeswehr University Munich, 85577 Neubiberg, Germany

Funder

China Scholarship Council

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.G006219

Reference24 articles.

1. ReveleyM. S.BriggsJ. L.EvansJ. K.SandiferC. E.JonesS. M. “Causal Factors and Adverse Conditions of Aviation Accidents and Incidents Related to Integrated Resilient Aircraft Control,” NASA TM-2010-216261, 2010.

2. Aircraft Loss of Control Problem Analysis and Research Toward a Holistic Solution

3. Evaluation of Aircraft Performance and Maneuverability by Computation of Attainable Equilibrium Sets

4. Aircraft Flight Envelope Determination Using Upset Detection and Physical Modeling Methods

5. Reachability and Region of Attraction Analysis Applied to GTM Dynamic Flight Envelope Assessment

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