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Results: 1-22 |
Results: 22
CONCATENATED APPROACH TO TRAJECTORY OPTIMIZATION
Authors: SEYWALD H KUMAR RR
Citation: H. Seywald et Rr. Kumar, CONCATENATED APPROACH TO TRAJECTORY OPTIMIZATION, Journal of guidance, control, and dynamics, 20(3), 1997, pp. 617-621
IDENTIFICATION OF THE OPTIMAL SWITCHING STRUCTURE FOR RANGE-OPTIMAL ATMOSPHERIC FLIGHT TRAJECTORIES
Authors: SEYWALD H
Citation: H. Seywald, IDENTIFICATION OF THE OPTIMAL SWITCHING STRUCTURE FOR RANGE-OPTIMAL ATMOSPHERIC FLIGHT TRAJECTORIES, Optimal control applications & methods, 18(3), 1997, pp. 159-177
METHOD FOR AUTOMATIC COSTATE CALCULATION
Authors: SEYWALD H KUMAR RR
Citation: H. Seywald et Rr. Kumar, METHOD FOR AUTOMATIC COSTATE CALCULATION, Journal of guidance, control, and dynamics, 19(6), 1996, pp. 1252-1261
VARIATIONAL SOLUTIONS FOR THE HEAT-RATE-LIMITED AEROASSISTED ORBITAL TRANSFER PROBLEM
Authors: SEYWALD H
Citation: H. Seywald, VARIATIONAL SOLUTIONS FOR THE HEAT-RATE-LIMITED AEROASSISTED ORBITAL TRANSFER PROBLEM, Journal of guidance, control, and dynamics, 19(3), 1996, pp. 686-692
SHOULD CONTROLS BE ELIMINATED WHILE SOLVING OPTIMAL-CONTROL PROBLEMS VIA DIRECT-METHODS
Authors: KUMAR RR SEYWALD H
Citation: Rr. Kumar et H. Seywald, SHOULD CONTROLS BE ELIMINATED WHILE SOLVING OPTIMAL-CONTROL PROBLEMS VIA DIRECT-METHODS, Journal of guidance, control, and dynamics, 19(2), 1996, pp. 418-423
DENSE-SPARSE DISCRETIZATION FOR OPTIMIZATION AND REAL-TIME GUIDANCE
Authors: KUMAR RR SEYWALD H
Citation: Rr. Kumar et H. Seywald, DENSE-SPARSE DISCRETIZATION FOR OPTIMIZATION AND REAL-TIME GUIDANCE, Journal of guidance, control, and dynamics, 19(2), 1996, pp. 501-503
FINITE-DIFFERENCE SCHEME FOR AUTOMATIC COSTATE CALCULATION
Authors: SEYWALD H KUMAR RR
Citation: H. Seywald et Rr. Kumar, FINITE-DIFFERENCE SCHEME FOR AUTOMATIC COSTATE CALCULATION, Journal of guidance, control, and dynamics, 19(1), 1996, pp. 231-239
LONG FLIGHT-TIME RANGE-OPTIMAL AIRCRAFT TRAJECTORIES
Authors: SEYWALD H
Citation: H. Seywald, LONG FLIGHT-TIME RANGE-OPTIMAL AIRCRAFT TRAJECTORIES, Journal of guidance, control, and dynamics, 19(1), 1996, pp. 242-244
SHORT COMMUNICATIONS ON THE EXISTENCE OF TOUCH POINTS FOR FIRST-ORDERSTATE INEQUALITY CONSTRAINTS
Authors: SEYWALD H CLIFF EM
Citation: H. Seywald et Em. Cliff, SHORT COMMUNICATIONS ON THE EXISTENCE OF TOUCH POINTS FOR FIRST-ORDERSTATE INEQUALITY CONSTRAINTS, Optimal control applications & methods, 17(5), 1996, pp. 357-366
FINITE-ELEMENT METHOD FOR THE SOLUTION OF STATE-CONSTRAINED OPTIMAL-CONTROL PROBLEMS
Authors: BLESS RR HODGES DH SEYWALD H
Citation: Rr. Bless et al., FINITE-ELEMENT METHOD FOR THE SOLUTION OF STATE-CONSTRAINED OPTIMAL-CONTROL PROBLEMS, Journal of guidance, control, and dynamics, 18(5), 1995, pp. 1036-1043
FUEL-OPTIMAL STATIONKEEPING VIA DIFFERENTIAL-INCLUSIONS
Authors: KUMAR RR SEYWALD H
Citation: Rr. Kumar et H. Seywald, FUEL-OPTIMAL STATIONKEEPING VIA DIFFERENTIAL-INCLUSIONS, Journal of guidance, control, and dynamics, 18(5), 1995, pp. 1156-1162
3-DIMENSIONAL AIR-TO-AIR MISSILE TRAJECTORY SHAPING
Authors: KUMAR RR SEYWALD H CLIFF EM KELLEY HJ
Citation: Rr. Kumar et al., 3-DIMENSIONAL AIR-TO-AIR MISSILE TRAJECTORY SHAPING, Journal of guidance, control, and dynamics, 18(3), 1995, pp. 449-456
NEAR-OPTIMAL 3-DIMENSIONAL AIR-TO-AIR MISSILE GUIDANCE AGAINST MANEUVERING TARGET
Authors: KUMAR RR SEYWALD H CLIFF EM
Citation: Rr. Kumar et al., NEAR-OPTIMAL 3-DIMENSIONAL AIR-TO-AIR MISSILE GUIDANCE AGAINST MANEUVERING TARGET, Journal of guidance, control, and dynamics, 18(3), 1995, pp. 457-464
GENETIC ALGORITHM APPROACH FOR OPTIMAL-CONTROL PROBLEMS WITH LINEARLYAPPEARING CONTROLS
Authors: SEYWALD H KUMAR RR DESHPANDE SM
Citation: H. Seywald et al., GENETIC ALGORITHM APPROACH FOR OPTIMAL-CONTROL PROBLEMS WITH LINEARLYAPPEARING CONTROLS, Journal of guidance, control, and dynamics, 18(1), 1995, pp. 177-182
ARTIFICIAL NEURAL NETWORKS IN-SPACE STATION OPTIMAL ATTITUDE-CONTROL
Authors: KUMAR RR SEYWALD H DESHPANDE SM RAHMAN Z
Citation: Rr. Kumar et al., ARTIFICIAL NEURAL NETWORKS IN-SPACE STATION OPTIMAL ATTITUDE-CONTROL, Acta astronautica, 35(2-3), 1995, pp. 107-117
NEIGHBORING OPTIMAL-CONTROL BASED FEEDBACK LAW FOR THE ADVANCED LAUNCH SYSTEM
Authors: SEYWALD H CLIFF EM
Citation: H. Seywald et Em. Cliff, NEIGHBORING OPTIMAL-CONTROL BASED FEEDBACK LAW FOR THE ADVANCED LAUNCH SYSTEM, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1154-1162
TRAJECTORY OPTIMIZATION-BASED ON DIFFERENTIAL INCLUSION
Authors: SEYWALD H
Citation: H. Seywald, TRAJECTORY OPTIMIZATION-BASED ON DIFFERENTIAL INCLUSION, Journal of guidance, control, and dynamics, 17(3), 1994, pp. 480-487
RANGE OPTIMAL TRAJECTORIES FOR AN AIRCRAFT FLYING IN THE VERTICAL PLANE
Authors: SEYWALD H CLIFF EM WELL KH
Citation: H. Seywald et al., RANGE OPTIMAL TRAJECTORIES FOR AN AIRCRAFT FLYING IN THE VERTICAL PLANE, Journal of guidance, control, and dynamics, 17(2), 1994, pp. 389-398
MINIMUM FUEL SPACECRAFT REORIENTATION
Authors: SEYWALD H KUMAR RR DESHPANDE SS HECK ML
Citation: H. Seywald et al., MINIMUM FUEL SPACECRAFT REORIENTATION, Journal of guidance, control, and dynamics, 17(1), 1994, pp. 21-29
NEW PROOF OF THE JACOBI NECESSARY CONDITION
Authors: SEYWALD H KUMAR RR CLIFF EM
Citation: H. Seywald et al., NEW PROOF OF THE JACOBI NECESSARY CONDITION, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1178-1181
SINGULAR CONTROL IN MINIMUM-TIME SPACECRAFT REORIENTATION
Authors: SEYWALD H KUMAR RR
Citation: H. Seywald et Rr. Kumar, SINGULAR CONTROL IN MINIMUM-TIME SPACECRAFT REORIENTATION, Journal of guidance, control, and dynamics, 16(4), 1993, pp. 686-694
GODDARD PROBLEM IN PRESENCE OF A DYNAMIC PRESSURE LIMIT
Authors: SEYWALD H CLIFF EM
Citation: H. Seywald et Em. Cliff, GODDARD PROBLEM IN PRESENCE OF A DYNAMIC PRESSURE LIMIT, Journal of guidance, control, and dynamics, 16(4), 1993, pp. 776-781
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