Perturbed Lambert Problem

The Perturbed Lambert Problem is a variant of the classical Lambert's Problem in orbital mechanics that incorporates perturbing forces—such as gravitational anomalies, atmospheric drag, or third-body effects—into the boundary value problem for determining spacecraft trajectories between two position vectors within a specified time of flight.

26

Publications

698

Citations

53

Authors

26

Institutions

Publications per year

2017–2026

10

Authors

53

  1. RP
    Ryan P. Russell

    The University of Texas at Austin, United States

    4 publications · 80 citations

    4

    h-index

  2. JL
    John L. Junkins

    Texas A&M University, United States

    4 publications · 127 citations

    4

    h-index

  3. RW
    Robyn Woollands

    Texas A&M University, United States

    3 publications · 78 citations

    3

    h-index

  4. YL
    Ya-Zhong Luo

    National University of Defense Technology, China

    2 publications · 112 citations

    2

    h-index

  5. JL
    Julie L. Read

    Texas A&M University, United States

    2 publications · 34 citations

    2

    h-index

1–5 of 53

Venues

  1. Journal of Guidance Control and Dynamics

    11 publications · 361 citations

    11

    h-index

  2. Celestial Mechanics and Dynamical Astronomy

    4 publications · 97 citations

    4

    h-index

  3. The Journal of the Astronautical Sciences

    3 publications · 50 citations

    3

    h-index

  4. NASA Technical Reports Server (NASA)

    Repository · 1 publications · 56 citations

    1

    h-index

  5. Journal of Spacecraft and Rockets

    1 publications · 14 citations

    1

    h-index

1–5