Nonlinear autopilot for high maneuverability of bank-to-turn missiles

IEEE Transactions on Aerospace and Electronic Systems

Volumn 37, Issue 4, 2001, Pages 1236-1253

  Lee, Sang Yong ^a   Lee, Ju Il ^b   In Joong, H A ^c,d  

^a Samsung Advanced Institute of Technology (SAIT)   (South Korea)

^b SAMSUNG Electronics   (South Korea)

^c Seoul National University   (South Korea)

^d Department of Aerospace Engineering   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; FEEDBACK CONTROL; LINEARIZATION; MANEUVERABILITY; PERTURBATION TECHNIQUES; SYSTEMS ANALYSIS;

NONLINEAR AUTOPILOTS;

MISSILES;

EID: 0035493483     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/7.976962     Document Type: Article

References (21)

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3. Modern control theory for design of autopilots for bank-to-turn missiles
4. Autopilot design for bank-to-turn missiles using LQG/LTR methodology
5. Gain scheduling for H-infinity controllers: A flight control example
6. Gain-scheduled bank-to-turn autopilot design using linear parameter raring transformation
7. Nonlinear autopilot and guidance for a highly maneuverable missile
8. Adaptive robust bank-to-turn missile autopilot design using neural networks
9. Hybrid neural adaptive control for bank-to-turn missile
10. Missile autopilot design via functional inversion and time-scaled transformation
11. Autopilot design for highly maneuvering STT missiles via singular preturbation-like technique
12. The standard decomposed system and noninteracting feedback control of nonlinear systems
13. Singular perturbations and time scales in guidance, navigation and control of aerospace systems: Survey
14. Nondimensional forms for singular perturbation analyses of aircraft energy climbs