Development and Evaluation of Control Architectures for a Mechanically Deployed Entry Vehicle
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
2. Johns Hopkins University, Applied Physics Laboratory, Laurel, Maryland 20723
3. NASA Johnson Space Center, Houston, Texas 77058
Funder
NASA Space Technology Mission Directorate
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A35255
Reference13 articles.
1. Alternate Trimming Methods for Trailing Aircraft in Formation Flight
2. Experimental Hypersonic Aerodynamic Characteristics of Mars Surveyor 2001 Precision Lander with Flap
3. Moving mass trim control for aerospace vehicles
4. Integrated Guidance and Control of Moving-Mass Actuated Kinetic Warheads
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