The Online Books Page

Optimal control

See also what's at your library, or elsewhere.

• Necessary conditions for optimal lunar trajectories with discontinuous state variables and intermediate point constraints (National Aeronautics and Space Administration ;, 1967), by W. E. Miner, J. F. Landrus, Northrop Space Laboratories, and Electronics Research Center (U.S.) (page images at HathiTrust)
• An algorithm for Liapunov stability analysis of complex nonlinear systems with application to the Orbiting Astronomical Observatory (National Aeronautics and Space Administration ;, 1971), by Gunther R. Geiss, Ames Research Center, and Grumman Aerospace Corporation (page images at HathiTrust)
• Fundamental limitations on V/STOL terminal guidance due to aircraft characteristics (National Aeronautics and Space Administration ;, 1971), by Julian Wolkovitch, D. William Lochtie, Charles W. LaMont, Lewis Research Center, and inc Mechanics Research (page images at HathiTrust)
• Minimum fuel attitude control of a nonlinear satellite system with bounded control by a method based on linear programming (National Aeronautics and Space Administration ;, 1969), by Gary D. Wolske, Irmgard Flügge-Lotz, United States National Aeronautics and Space Administration, and Stanford University (page images at HathiTrust)
• Approximate optimal guidance for the advanced launch system (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993), by T. S. Feeley, J. L. Speyer, United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, and Langley Research Center (page images at HathiTrust)

Items below (if any) are from related and broader terms.