[Free] NONLINEAR AUTOPILOT DESIGN FOR AEROSPACE VEHICLES: NONLINEAR DESIGN OF 3-AXES AUTOPILOT FOR SHORT RANGE SKID-TO-TURN HOMING MISSILES
▲ Abhijit Das, Siddhartha Mukhopadhyay ▲
| #1977641 in Books | 2010-03-04 | Original language:English | PDF # 1 | 8.66 x.52 x5.91l,.75 | File Name: 3639241207 | 228 pages
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Traditionally, missile autopilots have been designed using linear control approaches with gain scheduling. Moreover, three single axis autopilots are usually designed without considering the interaction among the motion axes. Such designs cannot handle the coupling among pitch-yaw-roll channels, especially under high angles of attack occurring in high maneuver zones. In most research studies, realistic factors like fin saturation, limitation of gimbal freedom etc are no...
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