A near optimal midcourse guidance law based on spherical gravity

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Deihoul, Ali Reza ^a,b   Massoumnia, Mohammad Ali ^a,c  

^a SHARIF UNIVERSITY OF TECHNOLOGY   (Iran)

^b School of Electrical Engineering   (Iran)

^c Department of Electrical Engineering ^*  (Iran)

Author keywords

[No Author keywords available]

Indexed keywords

BALLISTIC MISSILES;

CLOSED FORM SOLUTIONS; DEGRADED PERFORMANCE; GRAVITY MODEL; MATRIX COEFFICIENTS; MIDCOURSE GUIDANCE; OPTIMIZATION PROBLEMS; REAL PROBLEMS; RELATIVE MOTION;

GUIDED MISSILES;

EID: 85086614473     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4840     Document Type: Conference Paper

References (3)

1. Mohammad-Ali Massoumnia, "Optimal Midcourse Guidance Law for Fixed-Interval Propulsive Maneuvers", Journal Of Guidance, Control, and Dynamics, Vol. 18, No.3, May-June, pp. 465-470, (1995).
2. R. H. Battin, "An Introduction to the Mathematics and Methods of Astrodynamics", AIAA Education Series, (1987).
3. Brett Newman, "Strategic Intercept Midcourse Guidance Using Modified Zero Effort Miss Steering", Journal Of Guidance, Control, and Dynamics, Vol. 19, No.1, January-February, pp. 107-112, (1996)