Project Summary
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Proposal Number: 970114
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Project Title: Intelligent, Gain Scheduled, Differential Throttling,
H? Control of Aerospike Space Transportation Systems
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Small Business Concern:
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American GNC Corporation
9131 Mason Avenue
Chatsworth, CA 91311
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Research Institution:
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University of Southern California
3440 S Hope St.
Los Angeles, CA 90089-2563
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Principal Investigator/Project Manager:
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Ching-Fang Lin
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Technical Abstract:
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NASA is considering the Single Stage To Orbit (STTO) concept. The
breakthrough technology of aerospike engines has made rocket propulsion
so much more efficient that STTO vehicles can now be seriously
considered in a foreseeable future. Both the X-33 and the Venture Star
will be equipped with aerospike engines. However, aerospike engines
pose new control challenges -- they cannot be gimballed like
conventional rocket engines; they are fixed relative to the rocket
structure; therefore, aerospike engine rockets will have to be
controlled by differential throttling. This project is aimed to
transfer our experience and techniques in Propulsion Controlled
Aircraft (PCA) control system design to NASA and solve this challenging problem. Especially, a multilevel aerospike space transportation control system based on H? model matching, and topological, intelligent, robust/nonlinear gain scheduling control will be designed to ensure good performance of the control system over the whole flight
envelope. Design and analysis algorithms will be developed
and a software environment with a graphical user interface will be
implemented to synthesize, simulate, and evaluate the designed control
system. Our experience makes us uniquely qualified to design the
differential throttling control system of such advanced aerospike space
transportation systems as the X-33 and Venture Star.
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Potential Commercial Applications:
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With the commercialization of space afforded by aerospike engines, the
need for "fly-by-throttle" concepts will be increasing. With more and
more sophesticated aeropace structures being considered -- stealth
aircraft without vertical fins, flying wings -- that do not have
conventional control surfaces but that will be flown by pilots used to
fly aircraft with conventional control surfaces, the need to make
these structures "feel" like a conventional aircraft will make our
model matching concept more and more important.