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OPTIMAL FEEDBACK GUIDANCE FOR LOW‐THRUST ORBIT INSERTION

  • Published:1995-07 Issue:3 Volume:16 Page:155-173
  • ISSN:0143-2087
  • Container-title:Optimal Control Applications and Methods
  • language:en
  • Short-container-title:Optimal Control Applications and Methods

Author:

Kluever Craig A.1

Affiliation:

1. Mechanical and Aerospace EngineeringUniversity of Missouri—Kansas City5100 Rockhill RoadKansas CityMO64110U.S.A.

Publisher

Wiley

Subject

Applied Mathematics,Control and Optimization,Software,Control and Systems Engineering

Reference12 articles.

1. Comparison of potential electric propulsion systems for orbit transfer

2. Modular, ion-propelled, orbit-transfer vehicle

3. Optimum guidance for a low thrust interplanetary vehicle.

4. Korsmeyer D. J. ‘A cislunar guidance methodology and model for low thrust trajectory generation’ AAS Paper 91–433 1991.

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