SDRE based guidance law for impact angle constrained trajectories

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2007

Volumn 3, Issue , 2007, Pages 2202-2217

  Ratnoo, Ashwini ^a,b   Ghose, Debasish ^a,b  

^a INDIAN INSTITUTE OF SCIENCE   (India)

^b Department of Aerospace Engineering ^*  (India)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CONSTRAINT THEORY; PROBLEM SOLVING; ROBUSTNESS (CONTROL SYSTEMS);

CONSTRAINED TRAJECTORIES; GUIDANCE LAW; IMPACT ANGLES; PLANAR ENGAGEMENTS; REALISTIC MISSILE MODELS;

TRAJECTORIES;

EID: 37249003746     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-6539     Document Type: Conference Paper

References (15)

1. M. Kim and K.V. Grider: Termainal Guidance For Impact Attitude Angle Costrained Flight Trajetories, IEEE Transactions on Aerospace and Electronic Systems, AES-9, 6 (Dec. 1973). 852-859.
2. R.J. York and H.L. Pastrick: Optimal terminal guidance with constraints at final time, Journal of Spacecraft and Rockets, 14 (June 1977), 381-382.
3. B.S. Kim, J.G. Lee and H.S. Han: Biased PNG law for impact with angular constraint, JIEEE Transactions on Aerospace and Electronic Systems,AES-34, 1(Jan. 1998), 277-288.
4. C.K. Ryoo, H. Cho and M.J. Tahk:Optimal guidnace laws with terminal impact angle constraint, Journal of Guidance, Control, and Dynamics, Vol.28 No.4, July-August 2005, 724-732.
5. J. R. Cloutier: State-Dependent Riccati Equation Techniques: An Overview, Proceedings of the American Control Conference New-Mexico, June 1997, 932-936.
6. J. R. Cloutier, Donald T. Stansbery: The Capabilities and Art of State-Dependent Riccati Equation-Based Design, Proceedings of the American Control Conference Anchorage, AK, May 2002, 86-91.
7. J.R. Cloutier: Adaptive matched augmented proportional navigation, AIAA Missile Sciences Conference, 1994.
8. J. R. Cloutier: Time-to-go-less guidance with cross-channel couplings, Proceedings of the AIAA Missile sciences Conference Monterey, CA, December 1996.
9. J. R. Cloutier, P. H. Zipfel: Hypersonic Guidance via the State-Dependent Riccati Equation Control Method, Proceedings of the 1999 IEEE International Conference on Control Applications Kohala Coast-Island of Hawaii, Hawaii, USA August 1999.
10. S.N. Balakrishnan, M. Xin: Robust State Dependent Riccati Equation Based Guidance laws, Proceedings of the American Control Conference Arlington VA June 25-27, 2001.
11. C. P. Mracek and J. R. Cloutier: Missile longitudinal autopilot design using the state-dependent Riccati equation method, In Proceedings of the International Conference on Nonlinear Problems in Aviation and Aerospace, Available through University Press, Embry- Riddle Aeronautical University, Daytona Beach, FL. 32114, May 1996.
12. C.P Mracek, J.R. Cloutier, and C.N. DSouza: A new technique for nonlinear estimation. Proceedings of the IEEE Conference on Control Applications Dearborn, MI, September 1996.
13. D. Ehrler and S.R. Vadali: Examination of the optimal nonlinear regulator problem, Proceedings of the AIAA Guidance. Navigation and Control Conference Minneapolis, MN, August 1988.
14. ∞ control via the state dependent Riccati equation technique; part 1, theory; part 2, Proceedings of the International Conference on Nonlinear Problems in Aviation and Aerospace May 1996.
15. P. E. Kee, L. Dong, and C. J. Siong: Near Optimal Midcourse Guidance Law for Flight Vehicle, Proceedings of 36th AIAA Aerospace Sciences Meeting and Exhibit Reno, NV, January 12-15.