Publication:
Performance, Control, and Simulation of the Affordable Guided Airdrop System

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Authors
Williams, T.
Hewgley, C.
Yakimenko, O.
Howard, R.
Kaminer, I.
Dellicker, S.
Benney, R.
Patel, S.
Subjects
AGAS
Aerodynamic Decelerator Systems Center
Advisors
Date of Issue
2000-08
Date
August 14-17, 2000
Publisher
American Institute of Aeronautics & Astronautics
Language
Abstract
This paper addresses the development of an autonomous guidance, navigation and control system for a flat solid circular parachute. This effort is a part of the Affordable Guided Airdrop System (AGAS) that integrates a low-cost guidance and control system into fielded cargo air delivery systems. The paper describes the AGAS concept, its architecture and components. It then reviews the literature on circular parachute modeling and introduces a simplified model of a parachute. This model is used to develop and evaluate the performance of a modified bang-bang control system to steer the AGAS along a pre-specified trajectory towards a desired landing point. The synthesis of the optimal control strategy based on Pontryagin's principle of optimality is also presented. The paper is intended to be a summary of the current state of AGAS development. The paper ends with the summary of the future plans in this area.
Type
Conference Paper
Description
Series/Report No
Department
Organization
Naval Postgraduate School (U.S.)
Identifiers
NPS Report Number
Sponsors
Funder
Format
11 p.
Citation
Dellicker, S., Benney, R., Patel, S., Williams, T., Hewgley, C., Yakimenko, O., Howard, R., and Kaminer, I., “Performance, Control, and Simulation of the Affordable Guided Airdrop System,” Proceedings of the AIAA Guidance, Navigation, and Control Conference, Denver, CO, August 14-17, 2000.
Distribution Statement
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
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