Guidance Law for an Air-Breathing Launch Vehicle Using Predictive Control Concept
Author:
Affiliation:
1. Vikram Sarabhai Space Centre, Thiruvananthapuram 695 022, India
2. Noorul Islam College of Engineering, Thuckalay 629 175, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.23221
Reference7 articles.
1. Automated trajectory synthesis for hypersonic vehicles using energy management and variational calculus techniques
2. Control strategy for maximizing reconnaissance range of hypersonic cruise vehicles
3. Direct trajectory optimization using nonlinear programming and collocation
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