Self-tuning Guidance Applied To Aeroassisted Orbit Transfer Problems

S. N. Balakrishnan; Sri Gouri Iiamarsu

doi:10.2514/6.1992-4644

Self-tuning Guidance Applied To Aeroassisted Orbit Transfer Problems

S. N. Balakrishnan
, Sri Gouri Iiamarsu

Missouri University of Science and Technology

Research output: Contribution to journal › Article › peer-review

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.

Original language	American English
Journal	Astrodynamics Conference, 1992
DOIs	https://doi.org/10.2514/6.1992-4644
State	Published - Jan 1 1992

Disciplines

Aerospace Engineering
Mechanical Engineering

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title = "Self-tuning Guidance Applied To Aeroassisted Orbit Transfer Problems",

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.",

author = "Balakrishnan, \{S. N.\} and Iiamarsu, \{Sri Gouri\}",

year = "1992",

month = jan,

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doi = "10.2514/6.1992-4644",

language = "American English",

journal = "Astrodynamics Conference, 1992",

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AU - Balakrishnan, S. N.

AU - Iiamarsu, Sri Gouri

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Y1 - 1992/1/1

N2 - 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.

AB - 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.

UR - https://scholarsmine.mst.edu/mec_aereng_facwork/5311

UR - https://doi.org/10.2514/6.1992-4644

U2 - 10.2514/6.1992-4644

DO - 10.2514/6.1992-4644

M3 - Article

JO - Astrodynamics Conference, 1992

JF - Astrodynamics Conference, 1992

ER -

Self-tuning Guidance Applied To Aeroassisted Orbit Transfer Problems

Abstract

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