Integrated guidance and control of missiles with θ-D method

IEEE Transactions on Control Systems Technology

Volumn 14, Issue 6, 2006, Pages 981-992

  Xin, Min ^a   Balakrishnan, S N ^b   Ohlmeyer, Ernest J ^c  

^a MISSISSIPPI STATE UNIVERSITY   (United States)

^b University of Missouri Rolla   (United States)

^c Naval Surface Weapon Center   (United States)

Author keywords

Missile integrated guidance and control; Nonlinear systems; Optimal control

Indexed keywords

COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); FIRE CONTROL SYSTEMS; NONLINEAR CONTROL SYSTEMS; OPTIMAL CONTROL SYSTEMS;

AUTOPILOT DESIGN; GUIDANCE LAW; MISSILE INTEGRATED CONTROL; MISSILE INTEGRATED GUIDANCE;

MISSILES;

EID: 33750404299     PISSN: 10636536     EISSN: None     Source Type: Journal    
DOI: 10.1109/TCST.2006.876903     Document Type: Article

References (18)

1. C. F. Lin and W. R. Yueh, "Optimal controller for homing missiles," J. Guid., Contr., Dynamics, vol. 8, no. 3, pp. 408-411, May/Jun. 1985.
2. J. H. Evers, J. R. Cloutier, C. F. Lin, W. R. Yueh, and Q. Wang, "Application of integrated guidance and control schemes to a precision guided missile," in Proc. Amer. Contr. Conf., 1992, pp. 3225-3230.
3. P. K. Menon and E. J. Ohlmeyer, "Nonlinear integrated guidance and control laws for homing missiles," presented at the AIAA Guid., Nav. Contr. Conf. Exhibit, Montreal, ON, Canada, Aug. 2001, AIAA paper 2001-4160.
4. P. K Menon, G. D Sweriduk, E. J Ohlmeyer, and D. S. Malyevac, "Integrated guidance and control of moving-mass actuated kinetic warheads," J. Guid. Control Dyn., vol. 27, no. 1, pp. 118-126, Jan./ Feb. 2004.
5. A. Isidori, Nonlinear Control System, 3rd ed. Berlin, Germany: Springer-Verlag, 1995.
6. I. Shkolnikov and Y. Shtessel, "Integrated guidance-control system of a homing interceptor: sliding mode approach," presented at the AIAA Guid. Nav. Contr. Conf. Exhibit, Montreal, ON, Canada, Aug. 2001.
7. P. K Menon and E. J Ohlmeyer, "Integrated design of agile missile guidance and control systems," in Proc. 7th Mediterranean Conf. Contr. Autom., 1999, pp. 1469-1494.
8. J. R Cloutier, C. N D'Souza, and C. P Mracek, "Nonlinear regulation and nonlinear control via the state-dependent Riccati equation technique," in Proc. 1st Int. Conf. Nonlinear Problems Aviation Aerospace, 1996, pp. 117-123.
9. N. F Palumbo and T. D Jackson, "Integrated missile guidance and control: A state dependent Riccati differential equation approach," in Proc. IEEE Int. Conf. Contr. Appl., 1999, pp. 243-248.
10. M. Xin and S. N Balakrishnan, "A new method for suboptimal control of a class of nonlinear systems," Opt. Contr. Appl. Methods, vol. 26, no. 2, pp. 55-83, Mar./Apr. 2005.
11. M. Xin, S. N Balakrishnan, D. T Stansbery, and E. J Ohlmeyer, "Nonlinear missile autopilot design with theta-D technique," AIAA J. Guid. Control Dyn., vol. 27, no. 3, pp. 406-417, May/Jun. 2004.
12. A. E. Bryson and Y. C. Ho, Applied Optimal Control. Bristol, PA: Hemisphere, 1975.
13. P. K Menon and V. R Iragavarapu, "Robust nonlinear control technology for high-agility missile interceptors" (in Optimal Synthesis) Rep. 005, Jul. 1996, Prepared Under NSWCDD Phase I SBIR Contract.
14. J. R Cloutier and D. T Stansbery, "Control of a continuously stirred tank reactor using an asymmetric solution of the state-dependent Riccati equation," in Proc. IEEE Conf. Contr. Appl., 1999, pp. 893-898.
15. P. Zarchan, "Proportional navigation and weaving targets," J. Guid. Control Dyn., vol. 18, no. 5, pp. 969-974, Sep./Oct. 1995.
16. E. J. Ohlmeyer, "Root-mean-square miss distance of proportional navigation missile against sinusoidal target," J. Guid. Control, Dyn., vol. 19, no. 3, pp. 563-568, May-Jun. 1996.
17. W. R. Chadwick and P. Zarchan, "Interception of spiraling ballistic missiles," in Proc. Amer. Contr. Conf., 1995, pp. 4476-4483.
18. P. Zarchan, "Tracking and intercepting spiraling ballistic missiles," in Proc. IEEE PLANS 2000 Conf., 2000, pp. 277-284.