Self-tuning Guidance Applied To Aeroassisted Orbit Transfer Problems
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.
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
Mechanical and Aerospace Engineering
Article - Conference proceedings
© 2023 American Institute of Aeronautics and Astronautics, All rights reserved.
01 Jan 1992