Self-tuning Guidance Applied To Aeroassisted Orbit Transfer Problems

Author

S. N. Balakrishnan, Missouri University of Science and TechnologyFollow
Sri Gouri Iiamarsu

Abstract

A nonlinear self-tuning control method is used as a guidance law for the atmospheric portion of the aeroassisted maneuver. Nonlinear pole-placement method of selftuning control is used to track the reference trajectories during this period. Flight dynamics equations are formulated in a special form for generating the self-tuned control. Numerical examples from a coplanar reentry problems to illustrate the use of this method are presented.

Recommended Citation

S. N. Balakrishnan and S. G. Iiamarsu, "Self-tuning Guidance Applied To Aeroassisted Orbit Transfer Problems," Astrodynamics Conference, 1992, pp. 715 - 723, article no. AIAA-92-4644-CP, American Institute of Aeronautics and Astronautics, Jan 1992.

The definitive version is available at https://doi.org/10.2514/6.1992-4644

Department(s)

Mechanical and Aerospace Engineering

Document Type

Article - Conference proceedings

Document Version

Citation

File Type

text

Language(s)

English

Rights

© 2023 American Institute of Aeronautics and Astronautics, All rights reserved.

Publication Date

01 Jan 1992