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Volumn 19, Issue 2, 1996, Pages 418-423

Should controls be eliminated while solving optimal control problems via direct methods?

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; CALCULATIONS; CONSTRAINT THEORY; EQUATIONS OF MOTION; OPTIMAL CONTROL SYSTEMS; OPTIMIZATION; PROBLEM SOLVING;

EID: 0030108093     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/3.21634     Document Type: Article
Times cited : (24)

References (16)
  • 5
    • 0023382928 scopus 로고
    • Direct Trajectory Optimization Using Nonlinear Programming and Collocation
    • Hargraves, C. R., and Paris, S. W., "Direct Trajectory Optimization Using Nonlinear Programming and Collocation," Journal of Guidance, Control, and Dynamics, Vol. 10, No. 4, 1987, pp. 338-342.
    • (1987) Journal of Guidance, Control, and Dynamics , vol.10 , Issue.4 , pp. 338-342
    • Hargraves, C.R.1    Paris, S.W.2
  • 6
    • 0028425236 scopus 로고
    • Trajectory Optimization Based on Differential Inclusions
    • Seywald, H., "Trajectory Optimization Based on Differential Inclusions," Journal of Guidance, Control, and Dynamics, Vol. 17, No 3, 1994, pp. 480-487.
    • (1994) Journal of Guidance, Control, and Dynamics , vol.17 , Issue.3 , pp. 480-487
    • Seywald, H.1
  • 10
    • 84999115050 scopus 로고
    • Optimal and Suboptimal Minimum Time-to-Climb Trajectories
    • AIAA, Washington, DC, AIAA Paper 94-3554
    • Seywald, H., "Optimal and Suboptimal Minimum Time-to-Climb Trajectories," Proceedings of the AIAA Guidance, Navigation, and Control Conference, AIAA, Washington, DC, 1994, pp. 130-136 (AIAA Paper 94-3554).
    • (1994) Proceedings of the AIAA Guidance, Navigation, and Control Conference , pp. 130-136
    • Seywald, H.1
  • 12
    • 84999218661 scopus 로고
    • A Finite Difference Based Scheme for Automatic Costate Calculation
    • (Scottsdale, AZ), AIAA, Washington, DC, AIAA Paper 94-3583
    • Seywald, H., and Kumar, R. R., "A Finite Difference Based Scheme for Automatic Costate Calculation," Proceedings of the AIAA Guidance, Navigation, and Control Conference (Scottsdale, AZ), AIAA, Washington, DC, 1994, pp. 368-379 (AIAA Paper 94-3583).
    • (1994) Proceedings of the AIAA Guidance, Navigation, and Control Conference , pp. 368-379
    • Seywald, H.1    Kumar, R.R.2
  • 15
    • 0027627810 scopus 로고
    • Singular Control in Minimum Time Spacecraft Reorientation
    • Seywald, H., and Kumar, R. R., "Singular Control in Minimum Time Spacecraft Reorientation," Journal of Guidance, Control, and Dynamics, Vol. 16, No. 4, 1993, pp. 686-694.
    • (1993) Journal of Guidance, Control, and Dynamics , vol.16 , Issue.4 , pp. 686-694
    • Seywald, H.1    Kumar, R.R.2
  • 16
    • 85033813573 scopus 로고
    • Explicit Elimination of Linearly Appearing Controls
    • AAS Paper 95-176, Albuquerque, NM, Feb.
    • Seywald, H., and Kumar, R. R., "Explicit Elimination of Linearly Appearing Controls," 5th Annual AAS/AIAA Space Flight Mechanics Conf., AAS Paper 95-176, Albuquerque, NM, Feb. 1995.
    • (1995) 5th Annual AAS/AIAA Space Flight Mechanics Conf.
    • Seywald, H.1    Kumar, R.R.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.