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Inertial navigation (Astronautics)

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• Astrodynamics
• Astronautics
• Space vehicles -- Guidance systems

• Inertial navigation (Astronautics) -- Computer simulation
• Stellar inertial navigation systems

• Navigation, Inertial (Astronautics)

• Inertial navigation. (Van Nostrand, 1962), by Richard H. Parvin (page images at HathiTrust)
• Radio/optical/strapdown inertial guidance study for advanced kick-stage applications. Volume I, Summary. (National Aeronautics and Space Administration ;, 1969), by TRW Inc and Electronics Research Center (U.S.) (page images at HathiTrust)
• NASA TR R-137 (National Aeronautics and Space Administration ;, 1962), by Jerrold H. Suddath and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TR R-247 (National Aeronautics and Space Administration ;, 1966), by Peter R. Kurzhals, Carolyn Grantham, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Autonomous integrated GPS/INS navigation experiment for OMV : PHASE I feasibility study (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Triveni N. Upadhyay, Harley Rhodehamel, George J. Priovolos, George C. Marshall Space Flight Center, and Mayflower Communications Company (page images at HathiTrust)

• NASA TN D-4490 (National Aeronautics and Space Administration ;, 1968), by Robert D. Showman, G. Michael Sullivan, B. F. Doolin, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Sampled-data deviations in a vertical indicator with a stellar monitor (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Directorate of Systems Engineering, Air Research and Development Command, U.S. Air Force, 1960., 1960), by Thomas Michael Pienkowski, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (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)
• Techniques for generation of control and guidance signals derived from optical fields : Part II (National Aeronautics and Space Administration :, 1971), by H. Hemami, S. R. Gardner, R. B. McGhee, Langley Research Center, Ohio State University, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5843 (National Aeronautics and Space Administration ;, 1970), by Robert D. Showman, Bruce H. Dishman, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4490 (National Aeronautics and Space Administration ;, 1968), by Robert D. Showman, G. Michael Sullivan, B. F. Doolin, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Application of maximum likelihood techniques to the design of optimum star trackers (National Aeronautics and Space Administration ;, 1968), by Edwin C. Foudriat, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Celestial aspect sensor system (Hanscom AFB, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1975., 1975), by Russell G. Steeves, John Dulchinos, Henry A. Miranda, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Aspect determination for the AFGL infrared survey experiments (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1978., 1978), by Stephan D. Price, Russell G. Walker, Peter C. Tandy, Leonard P. Marcotte, Charles V. Cunniff, David S. Akerstrom, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• Pointing calibration of a high-resolution millimeter-wave antenna by star observations (L.G. Hansom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1971., 1971), by Melvin Burak and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Sampled-data deviations in a vertical indicator with a stellar monitor (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Directorate of Systems Engineering, Air Research and Development Command, U.S. Air Force, 1960., 1960), by Thomas Michael Pienkowski, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)

• Star tracker calibration (National Aeronautics and Space Administration ;, 1968), by Lawrence T. Draper, United States National Aeronautics and Space Administration, and Goddard Space Flight Center (page images at HathiTrust)

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

• An introduction to astrodynamics (Academic press, 1960), by Robert M. L. Baker and Maud Makemson (page images at HathiTrust)
• Modern flight dynamics. (Prentice-Hall, 1961), by W. Richard Kolk (page images at HathiTrust)
• Orbital dynamics of space vehicles. (Prentice-Hall, 1963), by Ralph Deutsch (page images at HathiTrust)
• Scientific findings from Explorer VI. ([For sale by the Superintendent of Documents, U. S. Govt. Print. Off.], 1965), by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Gravity fields of the solar system (National Aeronautics and Space Administration ;, 1975), by Alan Zendell, Samir Vincent, Richard D. Brown, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A study of the effect of man's motion on the attitude and orbital motion of a satellite. (Systems Engineering Group. Research and Technology Division, Air Force Systems Command, 1965), by Corrado R. Poli (page images at HathiTrust)
• Recent advances in astrodynamics, 1961 (University of California, 1962), by Robert M. L. Baker and Mary P. Francis (page images at HathiTrust)
• Two-impulse reorientation of asymmetric spacecraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by C. William Martz, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Theory of higher order optimum impulsive solutions (National Aeronautics and Space Administration, 1971), by J. F. Andrus (page images at HathiTrust)
• Optimum reentry trajectories of a lifting vehicle (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Jeng-Shing Chern, Nguyen X. Vinh, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• An exploratory statistical analysis of a planet approach-phase guidance schema using angular measurements with significant error (National Aeronautics and Space Administration :, 1960), by Alan L. Friedlander, David P. Harry, and Lewis Research Center (page images at HathiTrust)
• Minimal energy ballistic trajectories for manned and unmanned missions to Mercury (National Aeronautics and Space Administration, 1967), by Laurence Albert Manning (page images at HathiTrust)
• On a consistent system of astrodynamic constants (National Aeronautics and Space Administration, 1963), by Helmut G. L. Krause and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Astrodynamic constants analysis. (Air Force Cambridge Researh Laboratories, Office of Aerospace Research, U. S. Air Force, 1963), by Lockhead-California Company (page images at HathiTrust; US access only)
• Modern techniques in astrodynamics : an introduction (Wright-Patterson Air Force Base, Ohio : Aerospace Research Laboratories, Office of Aerospace Research, United States Air Force, 1970., 1970), by Lynn E. Wolaver and Aerospace Research Laboratories (U.S.) (page images at HathiTrust)
• Multiobjective optimization of aerospace structures (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, [1992], 1992), by R. V. Grandhi, Geetha Bharatram, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and Wright State University (page images at HathiTrust)

• Flight Mechanics/Estimation Theory Symposium 1990 : proceedings of a symposium sponsored by NASA Goddard Space Flight Center ... Greenbelt, Maryland, May 22-24, 1990 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990), by Flight Mechanics/Estimation Theory Symposium (1990 : Goddard Space Flight Center), Thomas Stengle, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight Mechanics symposium (National Aeronautics and Space Administration, Goddard Space Flight Center, 1997), by Flight Mechanics Symposium and Goddard Space Flight Center (page images at HathiTrust)
• Flight Mechanics/Estimation Theory Symposium 1992 : proceedings of a symposium sponsored by NASA Goddard Space Flight Center and held at Goddard Space Flight Center, Greenbelt, Maryland, May 5-7, 1992 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993), by Flight Mechanics/Estimation Theory Symposium (1992 : Goddard Space Flight Center), Thomas Stengle, and Goddard Space Flight Center (page images at HathiTrust)
• Structural dynamics and control interaction of flexible structures : proceedings of a workshop held at George C. Marshall Space Flight Center, Huntsville, Alabama, April 22-24, 1986 (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987), by Harold N. Scofield, Robert S. Ryan, George C. Marshall Space Flight Center, United States. Office of Aeronautics and Space Technology, and Workshop on Structural Dynamics and Control Interaction of Flexible Structures (1986 : Marshall Space Flight Center) (page images at HathiTrust)
• Structural dynamics and control of large space structures, 1982 : proceedings of a workshop held at NASA Langley Research Center, Hampton, Virginia, January 21-22, 1982 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by M. Larry Brumfield, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• NASA/DOD control/structures interaction technology, 1986 : proceedings of a conference sponsored by NASA Langley Research Center, Hampton, Virginia, and Air Force Wright Aeronautical Laboratories, Wright-Patterson AFB, Ohio, and held in Norfolk, Virginia, November 18-21, 1986 (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986), by Robert L. Wright, Air Force Wright Aeronautical Laboratories, Langley Research Center, United States Department of Defense, United States National Aeronautics and Space Administration, and Va.) NASA/DOD CSI Technology Conference (1st : 1986 : Norfolk (page images at HathiTrust)
• Flight mechanics/estimation theory symposium, 1989 : proceedings of a symposium sponsored by NASA Goddard Space Flight Center andheld at Goddard Space Flight Center, Greenbelt, Maryland, May 23-24, 1989 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989), by Flight Mechanics/Estimation Theory Symposium (1989 : Goddard Space Flight Center), Thomas Stengle, and Goddard Space Flight Center (page images at HathiTrust; US access only)

• Automated dynamic analytical model improvement (National Aeronatucs and Space Administration, Scientific and Technical Information Branch, 1981), by Alex Berman, Fu Shang Wei, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)

• Orbital dynamics of space vehicles. (Prentice-Hall, 1963), by Ralph Deutsch (page images at HathiTrust)
• Motion of artificial satellites in the Earth's gravitational field (National Aeronautics and Space Administration, for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1969), by I͡U. G. Evtushenko (page images at HathiTrust; US access only)
• Motion of an artificial satellite in an eccentric gravitation field (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1970), by V. G. Demin (page images at HathiTrust; US access only)
• CRRESRAD documentation (Hanscom Air Force Base, Massachusetts : Phillips Laboratory, Directorate of Geophysics, 1992., 1992), by Kevin J. Kerns, M. S. Gussenhoven, and USAF Phillips Laboratory. Geophysics Directorate (page images at HathiTrust)
• A study of the effect of man's motion on the attitude and orbital motion of a satellite. (Systems Engineering Group. Research and Technology Division, Air Force Systems Command, 1965), by Corrado R. Poli (page images at HathiTrust)
• Long-term orbital lifetime predictions (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by P. E. Dreher, A. T. Lyons, and George C. Marshall Space Flight Center. Missions Operations Laboratory (page images at HathiTrust)
• Orbit dynamics and geographical coverage capabilities of satellite-based solar occultation experiments for global monitoring of stratospheric constituents (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by David R. Brooks, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Decoupled control of a long flexible beam in orbit (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Harold A. Hamer, Katherine G. Johnson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Skylab orbital lifetime prediction and decay analysis (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by P. E. Dreher, G. Wittenstein, R. P. Little, George C. Marshall Space Flight Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Global matrix of thermospheric density values for selected solar/geomagnetic conditions and spacecraft orbital altitudes (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by D. L. Johnson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Delma C. Freeman, Bernard Spencer, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A feasibility study for Scout polar launches from NASA Wallops Flight Center (National Aeronautics and Space Administration ;, 1975), by T. R. Myler, Langley Research Center, and LTV Aerospace Corporation. Vought Systems Division (page images at HathiTrust)
• Drag coefficients for spheres in free molecular flow in O at satellite velocities (National Aeronautics and Space Administration ;, 1973), by John W. Boring, Robert R. Humphris, Langley Research Center, and University of Virginia (page images at HathiTrust)
• NASA TR R-147 (National Aeronautics and Space Administration ;, 1962), by Howard T. Phelan, United States National Aeronautics and Space Administration, and Goddard Space Flight Center (page images at HathiTrust)
• NASA TR R-148 (National Aeronautics and Space Administration ;, 1962), by William A. Mersman, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Theory of the secular variations in the orbit of a satellite of an oblate planet (U.S. G.P.O.], 1961), by William A. Mersman (page images at HathiTrust)
• NASA TR R-341 (National Aeronautics and Space Administration ;, 1970), by Abolghassem Ghaffari, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A discussion of Halphen's method for secular perturbations and its application to the determination of long range effects in the motions of celestial bodies. Part 1 (National Aeronautics and Space Administration, 1963), by Peter Musen, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5934 (National Aeronautics and Space Administration :, 1970), by George H. Born, James C. Kirkpatrick, Manned Spacecraft Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Derivation of Newtonian-type integration coefficients and some applications to orbit calculations (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by C. E. Velez and Jesse L. Maury (page images at HathiTrust; US access only)
• Nimbus II flight evaluation and engineering report, launch through orbit 5275 (National Aeronautics and Space Administration, 1969), by Joseph J. McNaney, Ralph Shapiro, Bennie A. Palmer, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Satellite and space propulsion systems (National Aeronautics and Space Administration, 1960), by Wolfgang E. Moeckel (page images at HathiTrust)
• An investigation of the fine-pointing control system of a soft-gimbaled orbiting telescope (National Aeronautics and Space Administration, 1970), by Frederick R. Morrell, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Tesseral harmonics of the gravitational field and geodetic datum shifts derived from camera observations of satellites (National Aeronautics and Space Administration, 1963), by William M. Kaula and Goddard Space Flight Center (page images at HathiTrust)
• NASA TN D-1745 (National Aeronautics and Space Administration, 1963), by Peter Musen, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• A Phase-locked phase filter for the minitrack system (National Aeronautics and Space Administration :, 1962), by Ronald F. Woodman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Determination of satellite orbits from radar data (National Aeronautics and Space Administration, 1960), by W. F. Cahill, Isadore Harris, and Goddard Space Flight Center (page images at HathiTrust)
• A modified Hansen's theory as applied to the motion of artificial satellites (National Aeronautics and Space Administration :, 1960), by Peter Musen and Goddard Space Flight Center (page images at HathiTrust)
• Development of the lunar and solar perturbations in the motion of an artificial satellite (National Aeronautics and Space Administration :, 1961), by P. Musen, E. Upton, A. Bailie, and Goddard Space Flight Center (page images at HathiTrust)
• NASA TN D-4104 (National Aeronautics and Space Administration ;, 1967), by James R. Ramler and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Estimates of minimum energy requirements for range-controlled return of a nonlifting satellite from a circular orbit (National Aeronautics and Space Administration, 1961), by Charles M. Jackson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Dynamics and column densities of small particles ejected from spacecraft (National Aeronautics and Space Administration ;, 1974), by Robert J. Naumann and George C. Marshall Space Flight Center. Space Sciences Laboratory (page images at HathiTrust)
• NASA TN D-6583 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), by Ward F. Hodge, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6584 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), by Bruce A. Conway, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Orbital flight handbook (Office of Scientific and Technical Information] National Aeronautics and Space Administration, 1963), by Martin Company. Space Systems Division, Donald Kraft, George Townsend, and George C. Marshall Space Flight Center (page images at HathiTrust)
• On the Harmonic analysis of absolute lunar elevations (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1966., 1966), by Donald H. Eckhardt and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Wind estimates near 150 km from the variation in inclination of low-perigee satellite orbits (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973), by J. M. Forbes and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• An empirical density model for predicting low-altitude satellite emphemerides (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1974., 1974), by J. M. Forbes, D. F. Gillette, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Space vehicle ephemeris and differential correction program unified theory. (Air Force Command and Control Development Division, Air Research and Development Command, U.S. Air Force, Laurence G. Hanscom Field, 1960), by Ford Motor Company. Aeronutronic. Astrodynamics Dept and United States. Air Force. Air Research and Development Command (page images at HathiTrust; US access only)

More items available under broader and related terms at left.