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Showing 1 to 2 of 2 for “"Entry simulation"”.

  1. Navigation analysis and design for Mars entry

    … system design for a lander module during entry at Mars. The system estimates the state vector with an extended Kalman filter, which utilizes update information provided by the following measurement types: two-way range with orbiting satellites, two-way Doppler with orbiting satellites, …

    mit Repository record for Navigation analysis and design for Mars entry (opens in a new tab)

  2. Assessment of application of the steep-lifting entry trajectory solution to real-time entry guidance

    … guidance applications. The steep-lifting entry trajectory solution is a set of closed-form analytical approximate solutions to the planar equations of motion, which includes expressions for range, flight-path angle, and altitude as functions of velocity. This thesis assesses the …

    uiuc Repository record for Assessment of application of the steep-lifting entry trajectory solution to real-time entry guidance (opens in a new tab)