Radar Cross Section Constraints in Flight-Path Optimization
Author:
Affiliation:
1. Royal Institute of Technology, SE-100 44 Stockholm, Sweden
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.3115
Reference13 articles.
1. Flight Testing an Optimal Trajectory for the Saab J35 Draken
2. Optimal Trajectory for a Minimum Fuel Turn
3. Flight Testing Radar Detection of the Saab 105 in Level Flight
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