New Proportional Navigation Law for Ground-to-Air Systems

Journal of Guidance, Control, and Dynamics

Volumn 26, Issue 5, 2003, Pages 822-825

  Ben Asher, Joseph Z ^a   Farber, Nathan ^b   Levinson, Sergei ^a  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

^b Wales Ltd   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; ELECTRONIC GUIDANCE SYSTEMS; MATHEMATICAL MODELS; OPTIMAL CONTROL SYSTEMS;

PROPORTIONAL NAVIGATION (PN) GUIDANCE;

AIR NAVIGATION;

EID: 0141973362     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.5118     Document Type: Article

References (4)

1. Zarchan,P., Tactical and Strategic Missile Guidance, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1990, Chap.8.
2. Ben-Asher,J.Z., and Yaesh,I., Advances in Missile Guidance Theory, Vol. 180. Progress in Astronautics and Aeronautics, AIAA, Reston. VA, 1998, pp. 25-88.
3. Speyer,J.L., Deyst,J., and Jacobson,D.A., "Optimization of Stochastic Linear Systems with Additive Measurement and Process Noise Using Exponential Performance Criteria," IEEE Transactions on Automatic Control, Vol. AC-19, No. 4, 1974, pp. 358-366.
4. Rhee,I., and Speyer,J.L., "A Game Theoretic Controller and Its Relationship to H-Infinity and Linear-Exponential-Gaussian Synthesis." IEEE Transactions on Automatic Control, Vol. AC-36, No. 9, 1991, pp. 1021-1032.