NDLI: Optimal guidance for hypersonic reentry using inversion and receding horizon control

Content Provider	IET Digital Library
Author	Cai, Wei wei Zhu, Yan wei Yang, Le ping Zhang, Yuan wen
Abstract	This study investigates the optimal guidance problem for reentry vehicles with focus on novel methods for nominal trajectory generation and tracking. To reduce the dimensionality of reentry trajectory optimisation problem, the inversion-based approach is utilised to partly eliminate the differential equations by reformulating the states and controls with some desired outputs. These outputs are parameterised with a mapped Chebyshev pseudospectral method, which is improved by conformal map and barycentric rational interpolation techniques in order to enhance the numerical accuracy for high-order derivatives of desired outputs. On the basis of the obtained nominal trajectory, a robust closed-loop guidance scheme is proposed using receding horizon control, whereas the associated two-point boundary value problem in each guidance cycle is readily solved by differential transformation method. Numerical simulations show that the proposed guidance scheme is feasible and effective for atmospheric reentry.
Starting Page	1347
Ending Page	1355
Page Count	9
ISSN	17518644
Volume Number	9
e-ISSN	17518652
Issue Number	Issue 9, Jun (2015)
Alternate Webpage(s)	https://digital-library.theiet.org/content/journals/iet-cta/9/9
Alternate Webpage(s)	https://digital-library.theiet.org/content/journals/10.1049/iet-cta.2014.1155
Journal	IET Control Theory & Applications
Publisher Date	2015-04-16
Access Restriction	Open
Rights Holder	© The Institution of Engineering and Technology
Subject Keyword	Aerospace Control Aircraft Barycentric Rational Interpolation Technique Boundary Value Problem Chebyshev Approximation Chebyshev Pseudospectral Method Conformal Map Interpolation Technique Differential Equation (numerical Analysis) Differential Transformation Method Hypersonic Reentry Interpolation And Function Approximation Inversion Horizon Control Nominal Trajectory Generation Nominal Trajectory Tracking Numerical Accuracy Numerical Analysis Numerical Simulation Optimal Control Optimal Guidance Problem Optimisation Optimisation Technique Receding Horizon Control Reentry Trajectory Optimisation Problem Reentry Vehicle Robust Closed-loop Guidance Scheme Trajectory Optimisation (aeroSpace)
Content Type	Text
Resource Type	Article
Subject	Control and Optimization Control and Systems Engineering Human-Computer Interaction Electrical and Electronic Engineering Computer Science Applications

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4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
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