Efficient Thrust Management Algorithm for Variable Thrust Solid Propulsion System with Multi-Nozzles
Author:
Affiliation:
1. Korea Advanced Institute of Science and Technology, Daejeon 34141, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Reference17 articles.
1. Efficient Thrust Distribution with Adaptive Pressure Control for Multinozzle Solid Propulsion System
2. Variable Thrust Solid Propulsion Control Using Labview
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4. Control system design and experiment of needle-type gas regulating system for ducted rocket
5. Robust Propulsion Control in all Flight Stages of a Throtteable Ducted Rocket
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