LEADER 04382nam 22007095 450 001 9911006877203321 005 20190708092533.0 010 $a9781680159295 010 $a1680159291 010 $a9781400880034 010 $a1400880033 024 7 $a10.1515/9781400880034 035 $a(CKB)3710000000485573 035 $a(EBL)4009383 035 $a(SSID)ssj0001552726 035 $a(PQKBManifestationID)16171561 035 $a(PQKBTitleCode)TC0001552726 035 $a(PQKBWorkID)13572315 035 $a(PQKB)10365700 035 $a(MiAaPQ)EBC4009383 035 $a(DE-B1597)467715 035 $a(OCoLC)1002232439 035 $a(OCoLC)1004874642 035 $a(OCoLC)1011461476 035 $a(OCoLC)1013963394 035 $a(OCoLC)946713568 035 $a(OCoLC)999371744 035 $a(DE-B1597)9781400880034 035 $a(PPN)26512932X 035 $a(FR-PaCSA)88935482 035 $a(Perlego)736274 035 $a(FRCYB88935482)88935482 035 $a(EXLCZ)993710000000485573 100 $a20190708d2015 fg 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aControl of Spacecraft and Aircraft /$fArthur E. Bryson 210 1$aPrinceton, NJ : $cPrinceton University Press, $d[2015] 210 4$dİ1994 215 $a1 online resource (406 p.) 300 $aDescription based upon print version of record. 311 08$a9780691087825 311 08$a0691087822 320 $aIncludes bibliographical references (pages [369-375]) and index. 327 $tFrontmatter -- $tContents -- $tList of Figures -- $tList of Tables -- $tPreface and Acknowledgments -- $tChapter 1. Natural Motions of Rigid Spacecraft -- $tChapter 2. Spacecraft Sensors and Attitude Determination -- $tChapter 3. Attitude Control with Thrusters -- $tChapter 4. Attitude Control with Reaction Wheels -- $tChapter 5. Attitude Stabilization with Spin -- $tChapter 6. Attitude Control with a Gimbaled Momentum Wheel -- $tChapter 7. Attitude Control during Thrust Maueuvers -- $tChapter 8. Control of Translational Motions -- $tChapter 9. Flexibility and Fuel Slosh -- $tChapter 10. Natural Motions of Rigid Aircraft -- $tChapter 11. Aircraft Seusors -- $tChapter 12. Control of Longitudinal Motions of Aircraft -- $tChapter 13. Control of Lateral Motions of Aircraft -- $tChapter 14. Control of Helicopters near Hover -- $tChapter 15. Aeroelastic Systems -- $tAppendix A. Linear System Representations -- $tAppendix B. Steady-State Control -- $tAppendix C. Synthesis of Analog Control Logic -- $tAppendix D. Synthesis of Digital Control Logic -- $tAppendix E. Simulation -- $tAppendix F. Modeling Flexible Systems -- $tReferences -- $tIndex 330 $aHere a leading researcher provides a comprehensive treatment of the design of automatic control logic for spacecraft and aircraft. In this book Arthur Bryson describes the linear-quadratic-regulator (LQR) method of feedback control synthesis, which coordinates multiple controls, producing graceful maneuvers comparable to those of an expert pilot. The first half of the work is about attitude control of rigid and flexible spacecraft using momentum wheels, spin, fixed thrusters, and gimbaled engines. Guidance for nearly circular orbits is discussed. The second half is about aircraft attitude and flight path control. This section discusses autopilot designs for cruise, climb-descent, coordinated turns, and automatic landing. One chapter deals with controlling helicopters near hover, and another offers an introduction to the stabilization of aeroelastic instabilities. Throughout the book there is a strong emphasis on the mathematical modeling necessary for designing a good feedback control system. The appendixes summarize analysis of linear dynamic systems, synthesis of analog and digital feedback control, simulation, and modeling of flexible vehicles. 606 $aSpace vehicles$xAttitude control systems 606 $aAirplanes$xControl systems 615 0$aSpace vehicles$xAttitude control systems. 615 0$aAirplanes$xControl systems. 676 $a629.45 686 $aZO 7230$2rvk 700 $aBryson$b Arthur E., $0728108 801 0$bDE-B1597 801 1$bDE-B1597 906 $aBOOK 912 $a9911006877203321 996 $aControl of spacecraft and aircraft$91422856 997 $aUNINA