LEADER 02436nam 2200589 a 450 001 9910810030203321 005 20230213212242.0 010 $a1-60086-787-1 010 $a1-60086-786-3 035 $a(CKB)2550000000072640 035 $a(EBL)3111510 035 $a(SSID)ssj0000630681 035 $a(PQKBManifestationID)12275927 035 $a(PQKBTitleCode)TC0000630681 035 $a(PQKBWorkID)10747120 035 $a(PQKB)10038585 035 $a(Au-PeEL)EBL3111510 035 $a(CaPaEBR)ebr10516614 035 $a(OCoLC)922978913 035 $a(MiAaPQ)EBC3111510 035 $a(EXLCZ)992550000000072640 100 $a20041104d1985 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 12$aA case study on the F-16 fly-by-wire flight control system$b[electronic resource] /$fby Carl S. Droste and James E. Walker 210 $a[New York] $cAmerican Institute of Aeronautics and Astronautics$d[1985?] 215 $a1 online resource (120 p.) 225 1 $aAIAA professional study series 300 $aDescription based upon print version of record. 311 $a1-56347-307-0 327 $a""Cover""; ""Title""; ""Table Of Contents""; ""List Of Figures""; ""List Of Table""; ""1. Introduction""; ""2. The F - 16 Design Philosophy""; ""3. Implementation Of The Flight Control System Design""; ""3.1 The Fly-By-Wire Decision""; ""3.2 The Electrical-To-Mechanical Interface""; ""3.3 Redundancy""; ""3.4 Lightning Protection""; ""4. Unique Flight Control System Functional Features""; ""4.1 Aoa/g Limiting""; ""4.2 High-Aoa Roll Coordination""; ""4.3 Roll Rate Limiter""; ""4.4 Rudder Fadeout""; ""4.5 Yaw Rate Limiter""; ""4.6 Manual Pitch Override""; ""5. Conclusions"" 410 0$aAIAA professional study series. 606 $aFlight control 606 $aF-16 (Jet fighter plane) 606 $aAirplanes$xControl systems 615 0$aFlight control. 615 0$aF-16 (Jet fighter plane) 615 0$aAirplanes$xControl systems. 676 $a629.135 700 $aDroste$b Carl S$0727767 701 $aWalker$b James E$0103898 712 02$aAmerican Institute of Aeronautics and Astronautics. 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910810030203321 996 $aA case study on the F-16 fly-by-wire flight control system$93913829 997 $aUNINA