Fuel-optimal Trajectories

Fuel-Optimal Trajectories is a trajectory optimization method that determines the minimum propellant consumption path for orbital transfers by leveraging impulsive maneuvers at apoapsis and periapsis, distinguishing it from other trajectory designs through its adherence to the principles of the Hohmann transfer as the most fuel-efficient two-impulse solution in coplanar circular orbits.

162

Publications

7.4K

Citations

356

Authors

137

Institutions

Publications per year

2017–2026

47

Authors

356

  1. JP
    Jonathan P. How

    Massachusetts Institute of Technology, United States

    5 publications · 820 citations

    5

    h-index

  2. FY
    Fred Y. Hadaegh

    Jet Propulsion Laboratory, United States

    5 publications · 182 citations

    5

    h-index

  3. DP
    Daniel P. Scharf

    Jet Propulsion Laboratory, United States

    5 publications · 275 citations

    5

    h-index

  4. BA
    Behçet Açıkmeşe

    University of Washington, United States

    5 publications · 659 citations

    5

    h-index

  5. SG
    Shengping Gong

    Tsinghua University, China

    5 publications · 109 citations

    5

    h-index

1–5 of 356

Venues

  1. Journal of Guidance Control and Dynamics

    49 publications · 3.1K citations

    28

    h-index

  2. 9

    h-index

  3. AIAA Journal

    5 publications · 229 citations

    5

    h-index

  4. 5

    h-index

  5. AIAA Guidance, Navigation, and Control Conference

    Conference · 4 publications · 189 citations

    4

    h-index

1–5