Approximate trajectory tracking of input-disturbed PVTOL aircraft with delayed attitude measurements

International Journal of Robust and Nonlinear Control

Volumn 20, Issue 14, 2010, Pages 1610-1621

  Zhu, Bo ^a   Wang, Xinhua ^a   Cai, Kai Yuan ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Input disturbances; Measurement delay; Non minimum phase; Output tracking; Pad approximation; Planar vertical take off and landing (PVTOL) aircraft; Sliding mode control

Indexed keywords

INPUT DISTURBANCE; MEASUREMENT DELAY; NON-MINIMUM PHASE; OUTPUT-TRACKING; SLIDING MODES; VERTICAL TAKE-OFF AND LANDINGS;

DELAY CONTROL SYSTEMS; FEEDBACK; LANDING; NONLINEAR FEEDBACK; SLIDING MODE CONTROL; STATE FEEDBACK; TAKEOFF;

AIRCRAFT CONTROL;

EID: 77957330463     PISSN: 10498923     EISSN: 10991239     Source Type: Journal    
DOI: 10.1002/rnc.1536     Document Type: Article

References (19)

1. Isidori A. Nonlinear Control Systems (3rd edn). Springer: London, 1995.
2. Devasia S, Chen D, Paden B. Nonlinear inversion-based output tracking. IEEE Transactions on Automatic Control 1996; 41:930-942.
3. Shkolnikov IA, Shtessel YB. Tracking controller design for a class of nonminimum-phase systems via the method of system center. IEEE Transactions on Automatic Control 2001; 46:1639-1643
4. Huang CS, Yuan K. Output tracking of nonlinear nonminimum phase PVTOL aircraft based on nonlinear state feedback control. International Journal of Control 2002; 75:466-473.
5. Al-Hiddabi SA, McClamroch NH. Tracking and maneuver regulation control for nonlinear non-minimum phase systems: application to flight control. IEEE Transactions on Control Systems Technology 2002; 10:780-792.
6. Wang XH, Yang G, Xu Wl. Output tracking for nonlinear nonminimum phase systems and application to PVTOL aircraft. International Journal of Systems Science 2008; 39:29-42.
7. Utkin VI. Sliding Modes in Control Optimization. Springer: Berlin, 1992.
8. Piergiovanni M, Liviu L, Walter AS. Time-delay effects on linear/nonlinear feedback control of simple aeroelastic systems. Journal of Guidance, Control, and Dynamics 2005; 28:53-62.
9. Liu HT, Brandel F. Compensator design for large time delay in a flight control system. AIAA Guidance, Navigation, and Control Conference and Exhibit, Providence, Phose Island, U.S.A., 2004; 46:16-19.
10. Smith RE, Sarrafian SK. Effect of time delay on flying qualities: an update. NASA Technical Memorandum 88264, August 1986.
11. Hauser J, Sastry S, Meyer G. Nonlinear control design for slightly nonminimum phase systems: application to V/STOL aircraft. Automatica 1992; 28:665-679.
12. Benvenuti L, Di Benedetto MD, Grizzle JW. Approximate output tracking for nonlinear nonminimum phase systems with an application to flight control. International Journal of Robust and Nonlinear Control 1993; 4:397-414.
13. Martin P, Devasia S, Paden B. A different look at output tracking: control of a VTOL aircraft. Proceedings of the CDC'94, Lake Buena Vista: FL, U.S.A., 1994; 2376-2381.
14. Sira-Ramirez H, Fliess M. Regulation of non-minimum phase outputs in a PVTOL aircraft. Proceedings of the CDC'98, Piscataway, NJ, U.S.A., 1998; 4222-4227.
15. Shkolnikov IA, Shtessel YB. Aircraft nonminimum phase control in dynamic sliding manifolds. Journal of Guidance, Control, and Dynamics 2001; 24:566-572.
16. Niemieca MP, Kravaris C. Nonlinear model-state feedback control for nonminimum-phase processes. Automatica 2003; 39:1295-1302.
17. Chen CT, Peng ST. A sliding mode control scheme for nonminimum phase non-linear uncertain input-delay chemical processes. Journal of Process Control 2006; 16:37-51.
18. Dorf R, Bishop R. Modern Control Systems. Addison-Wesley: Reading, MA, 1995.
19. Shtessel YB, Mirkin L, Palmor Z. Sliding mode control of nonlinear systems with time-delayed control using Padé approximation and Smith Predictor. Private Memorandum, vol.29, 2003.