OPTIMUM GUIDANCE FOR A LOW THRUST INTERPLANETARY VEHICLE

[1] BATTIN RH, 1964, ASTRONAUTICAL GUIDAN, P341

[2] THE OPTIMIZATION OF TRAJECTORIES [J]. JOURNAL OF THE SOCIETY FOR INDUSTRIAL AND APPLIED MATHEMATICS, 1959, 7 (02): : 215 - 247

[3] BREAKWELL JV, 1963, SIAM J CONTROL, V1, P193, DOI DOI 10.1137/0301011

[4] Kalman R., 1961, J BASIC ENG, V83, P95, DOI [10.1115/1.3658902, DOI 10.1115/1.3658902]

[5] GUIDANCE THEORY AND EXTREMAL FIELDS [J]. IRE TRANSACTIONS ON AUTOMATIC CONTROL, 1962, AC 7 (05): : 75 - &

[6] A TECHNIQUE FOR OPTIMAL FINAL VALUE CONTROL OF POWERED FLIGHT TRAJECTORIES [J]. AIAA JOURNAL, 1966, 4 (02) : 352 - &

[7] PFEIFFER CG, 1963, AIAA63267 PAP

[8] MAXIMUM LIKELIHOOD ESTIMATES OF LINEAR DYNAMIC SYSTEMS [J]. AIAA JOURNAL, 1965, 3 (08) : 1445 - &

[9] OPTIMUM ESTIMATION OF SATELLITE TRAJECTORIES INCLUDING RANDOM FLUCTUATIONS IN DRAG [J]. AIAA JOURNAL, 1965, 3 (04) : 717 - +

[10] LINEAR CONTROL THEORY APPLIED TO INTERPLANETARY GUIDANCE [J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1964, AC 9 (01) : 82 - &

[1] BATTIN RH, 1964, ASTRONAUTICAL GUIDAN, P341

[2] THE OPTIMIZATION OF TRAJECTORIES [J]. JOURNAL OF THE SOCIETY FOR INDUSTRIAL AND APPLIED MATHEMATICS, 1959, 7 (02): : 215 - 247

[3] BREAKWELL JV, 1963, SIAM J CONTROL, V1, P193, DOI DOI 10.1137/0301011

[4] Kalman R., 1961, J BASIC ENG, V83, P95, DOI [10.1115/1.3658902, DOI 10.1115/1.3658902]

[5] GUIDANCE THEORY AND EXTREMAL FIELDS [J]. IRE TRANSACTIONS ON AUTOMATIC CONTROL, 1962, AC 7 (05): : 75 - &

[6] A TECHNIQUE FOR OPTIMAL FINAL VALUE CONTROL OF POWERED FLIGHT TRAJECTORIES [J]. AIAA JOURNAL, 1966, 4 (02) : 352 - &

[7] PFEIFFER CG, 1963, AIAA63267 PAP

[8] MAXIMUM LIKELIHOOD ESTIMATES OF LINEAR DYNAMIC SYSTEMS [J]. AIAA JOURNAL, 1965, 3 (08) : 1445 - &

[9] OPTIMUM ESTIMATION OF SATELLITE TRAJECTORIES INCLUDING RANDOM FLUCTUATIONS IN DRAG [J]. AIAA JOURNAL, 1965, 3 (04) : 717 - +

[10] LINEAR CONTROL THEORY APPLIED TO INTERPLANETARY GUIDANCE [J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1964, AC 9 (01) : 82 - &