Iterative solution to differential geometric guidance problem

Aircraft Engineering and Aerospace Technology

Volumn 78, Issue 5, 2006, Pages 415-425

  Li, Chaoyong ^a   Jing, Wuxing ^a   Wang, Hui ^b   Qi, Zhiguo ^b  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

^b SHANGHAI ACADEMY OF SPACEFLIGHT TECHNOLOGY   (China)

Author keywords

Aircraft navigation; Control technology

Indexed keywords

AIR NAVIGATION; ALGORITHMS; ANGLE OF ATTACK INDICATORS; ELECTRONIC GUIDANCE SYSTEMS; ITERATIVE METHODS; TIME DOMAIN ANALYSIS; TRACKING (POSITION);

AIRCRAFT NAVIGATION; DIFFERENTIAL GEOMETRIC GUIDANCE; NEWTON ITERATIVE ALGORITHM; PROPORTIONAL NAVIGATION;

CONTROL SYSTEMS;

EID: 33749016463     PISSN: 00022667     EISSN: None     Source Type: Journal    
DOI: 10.1108/00022660610685800     Document Type: Article

References (15)

1. Adler, F.P. (1956), "Missile guidance by three-dimensional proportional navigation", Journal of Applied Physics, Vol. 27 No. 5, pp. 500-7.
2. Ariff, O., Zbikowski, R., Tsourdos, A. and White, B.A. (2004), "Differential geometric guidance based on the involute of the target's trajectory: 2-D aspects", Proceedings of the 2004 American Control Conference ACC'04, Boston, pp. 3640-4.
3. Ariff, O., Zbikowski, R., Tsourdos, A. and White, B.A. (2005), "Differential geometric guidance based on the involute of the target's trajectory", Journal of Guidance, Control and Dynamics, Vol. 28 No. 5, pp. 990-6.
4. Chiou, Y.C. and Kuo, C.Y. (1998), "Geometric approach to three-dimensional missile guidance problem", Journal of Guidance, Control and Dynamics, Vol. 21 No. 2, pp. 335-41.
5. Joseph, Z. and Asher, B. (2003), "New proportional navigation law for ground-to-air systems", Journal of Guidance Control and Dynamics, Vol. 23 No. 5, pp. 822-5.
6. Kuo, C.Y. and Chiou, Y.C. (2000), "Geometric analysis of missile guidance command", IEE Proc-Control Theory and Applications, Vol. 147 No. 2, pp. 205-11.
7. Kuo, C.Y., Soetanto, D. and Chiou, Y.C. (2001), "Geometric analysis of flight control command for tactical missile guidance", IEEE Transactions on Control System Technology, Vol. 9 No. 2, pp. 234-43.
8. Ortega, J.M. and Rheinboldt, W.C. (1970), Iterative Solution of Nonlinear Equations in Several Variables, Academic Press, New York, NY.
9. Sarkar, A.K., Tiwari, P.K. and Srinivasan, S. (2003), "Generalized PN guidance law for a practical pursuer evader engagement", Proceedings of 2003 AIAA Guidance, Navigation, and Control Conference and Exhibit, Austin, Texas, USA, AIAA Paper 2003-5651.
10. Siouris, G.M. (2004), Missile Guidance and Control Systems, Springer-Verlag, New York, NY.
11. Struik, D.J. (1998), Lectures on Classical Differential Geometry, Dover, New York, NY.
12. White, B.A., Zbikowski, R. and Tsourdos, A. (2005), "Direct intercept guidance using differential geometric concepts", Proceedings of 2005 AIAA Guidance, Navigation, and Control Conference and Exhibit, San Francisco, California, USA, AIAA Paper 2005-5969.
13. Zhang, Y. (1996), Flight Dynamics of Tactical Missile, Astronautics Book Concern, Beijing.
14. Zhang, Y-A., Hu, Y-A. and Lin, T. (2001), "Robust geometric approach to missile guidance", Chinese Journal of Control Theory and Application, Vol. 20 No. 1, pp. 13-20.
15. Zhang, Y-A., Hu, Y-A. and Su, S. (2002), "Geometric approach and robust control approach to three-dimensional missile guidance", Acta Aeronautica et Astronautica Sinica, Vol. 23 No. 1, pp. 88-90.