This technical report presents the results of preflight, postflight, and system improvement guidance and control analyses performed in support of the High Altitude Supersonic Target (HAST) KJ-4 flight test mission. The work that was performed consisted of analytical stability analyses and related simulation analysis studies. (Author)
High Altitude Supersonic Target (HAST) KJ-4 Guidance and Control System Analysis
1974
60 pages
Report
No indication
English
Missile Guidance & Control Systems , Guided missile targets , Guided missiles , Flight control systems , Computerized simulation , Automatic pilots , Guidance computers , Aerial targets , Performance(Engineering) , Airframes , Roll , Yaw , Pitch(Motion) , Guided missile launchers , Acceleration , Angle of attack , Dynamic response , Transfer functions , Damping , Supersonic flight , High altitude , Canard configuration , Ailerons , Maneuverability , Pitot tubes , Accelerometers , Telemetering data , Hybrid computers , KJ-4 guidance and control , High altitude supersonic target , HAST(High altitude supersonic targets) , Root locus method , Preflight analysis , Postflight analysis
High Altitude Supersonic Target (HAST), Phase II
NTIS | 1974
|High-altitude supersonic gas releases
Elsevier | 1982
|High-Altitude Turbulence For Supersonic Airplanes
NTRS | 1989
|High Altitude Supersonic Decelerator Test Vehicle
NTRS | 2013
|