Skip to main content
Top

2019 | OriginalPaper | Chapter

4. Trajectory Optimization

Author : James Miller

Published in: Planetary Spacecraft Navigation

Publisher: Springer International Publishing

Activate our intelligent search to find suitable subject content or patents.

search-config
loading …

Abstract

Navigation operations require the refinement of the design trajectory to obtain a high-precision trajectory for flight path control and science operations. The preliminary trajectory design often involves approximate solutions of boundary value problems that provide sufficient accuracy for mission design but are not accurate enough for flight operations. The final precision trajectory is obtained by driving a high-precision trajectory model with targeting and optimization algorithms that yield the final high-precision solution. The preliminary trajectory design provides an initial guess for starting the targeting algorithm. With experience, the preliminary design may sometimes be omitted and the trajectory design obtained directly by targeting.

Dont have a licence yet? Then find out more about our products and how to get one now:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

Springer Professional "Wirtschaft"

Online-Abonnement

Mit Springer Professional "Wirtschaft" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 340 Zeitschriften

aus folgenden Fachgebieten:

  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Versicherung + Risiko




Jetzt Wissensvorsprung sichern!

Literature
1.
go back to reference Bryson, A. E. and Yu-Chi Ho, Applied Optimal Control, Ginn Blaisdell Pub. Co., Waltham, MA., 1969. Bryson, A. E. and Yu-Chi Ho, Applied Optimal Control, Ginn Blaisdell Pub. Co., Waltham, MA., 1969.
2.
go back to reference Fletcher, R. and M.J.D. Powell, “A Rapidly Convergent Descent Method for Minimization”, Computer Journal, July, 1963.MATH Fletcher, R. and M.J.D. Powell, “A Rapidly Convergent Descent Method for Minimization”, Computer Journal, July, 1963.MATH
3.
go back to reference Hoffman, L. H. and R. N. Green,“Thrusting Trajectory Minimization Program for Orbital Transfer Maneuvers”, NASA TN d-1620, June 1971. Hoffman, L. H. and R. N. Green,“Thrusting Trajectory Minimization Program for Orbital Transfer Maneuvers”, NASA TN d-1620, June 1971.
4.
go back to reference Miller, J. K., “Determination of an Optimal Control for a Planetary Orbit Insertion Maneuver”, internal JPL document TM 392-94, July 20,1972. Miller, J. K., “Determination of an Optimal Control for a Planetary Orbit Insertion Maneuver”, internal JPL document TM 392-94, July 20,1972.
5.
go back to reference Miller, J. K., “A Parameter Search and Optimization Algorithm for the Viking Mars Orbit Insertion Maneuver”, internal JPL document IOM 392.5-747, April 11,1974. Miller, J. K., “A Parameter Search and Optimization Algorithm for the Viking Mars Orbit Insertion Maneuver”, internal JPL document IOM 392.5-747, April 11,1974.
6.
go back to reference Miller, J. K., “Determination of an Optimal Control Subject to Constraints by the Method of Explicit Functions”, internal JPL document EM 314–412, February 20,1987. Miller, J. K., “Determination of an Optimal Control Subject to Constraints by the Method of Explicit Functions”, internal JPL document EM 314–412, February 20,1987.
7.
go back to reference Miller, J. K., “Constrained Parameter Optimization by the Method of Explicit Functions: Application to MESSENGER Mission”, Paper AAS 05–174, 15th AAS/AIAA Space Flight Mechanics Conference, Copper Mountain,CO, January 23–27, 2005. Miller, J. K., “Constrained Parameter Optimization by the Method of Explicit Functions: Application to MESSENGER Mission”, Paper AAS 05–174, 15th AAS/AIAA Space Flight Mechanics Conference, Copper Mountain,CO, January 23–27, 2005.
8.
go back to reference Miller, J. K., “A Multiple Encounter Targeing and Optimization Algorithm”, AAS 05–336, AAS/AIAA Astrodynamics Specialist Conference, Lake Tahoe, CA, August 7, 2005. Miller, J. K., “A Multiple Encounter Targeing and Optimization Algorithm”, AAS 05–336, AAS/AIAA Astrodynamics Specialist Conference, Lake Tahoe, CA, August 7, 2005.
9.
go back to reference Pines, S., “An accelerated Version of the JPL-MOIOP Numerical Search Optimization Method”, Rep.No. 73–32, Analytical Mechanics Associates Inc., June, 1973 Pines, S., “An accelerated Version of the JPL-MOIOP Numerical Search Optimization Method”, Rep.No. 73–32, Analytical Mechanics Associates Inc., June, 1973
10.
go back to reference Pines, S., “A Direct Gradient Projection Method for Parameter Optimization with Nonlinear Constraints”, AMA Rep. No. 75-8, Analytical Mechanics Associates Inc., April, 1975 Pines, S., “A Direct Gradient Projection Method for Parameter Optimization with Nonlinear Constraints”, AMA Rep. No. 75-8, Analytical Mechanics Associates Inc., April, 1975
Metadata
Title
Trajectory Optimization
Author
James Miller
Copyright Year
2019
DOI
https://doi.org/10.1007/978-3-319-78916-3_4

Premium Partner