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Showing 1 to 15 of 15 for “"Reentry vehicle"”.

  1. On the linearized atmospheric contributions to reentry vehicle Cep

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1964.

    mit Repository record for On the linearized atmospheric contributions to reentry vehicle Cep (opens in a new tab)

  2. Terminal control of a variable-stability slender reentry vehicle

    … schemes are applied to a proposed slender reentry vehicle, controlled by two separately-articulating flaps. The flap deflections are summarized as symmetric and asymmetric flap deflections; the former manipulates the drag, lift-curve slope, and static margin; the latter controls the vehicle

    mit Repository record for Terminal control of a variable-stability slender reentry vehicle (opens in a new tab)

  3. Reentry Vehicle Aerodynamics and Control at Very High Angle of Attack

    In recent flight tests the X-38 reentry test vehicle spins during the deployment of the drogue parachute. An experimental aerodynamic study has been conducted at the University of Illinois using a scale model of the X-38 to explore the cause of this problem. A six-component sting balance was used …

    uiuc Repository record for Reentry Vehicle Aerodynamics and Control at Very High Angle of Attack (opens in a new tab)

  4. Precession damping and axial velocity control of a lightweight reentry vehicle

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.

    mit Repository record for Precession damping and axial velocity control of a lightweight reentry vehicle (opens in a new tab)

  5. Robust estimation and failure detection for reentry vehicle attitude control systems

    Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1998.

    mit Repository record for Robust estimation and failure detection for reentry vehicle attitude control systems (opens in a new tab)

  6. Boost through reentry trajectory planning for maneuvering reentry vehicles

    … rapidly planning a long range, boost-through- reentry mission, using a lightweight, highly maneuverable reentry vehicle. An Aimpoint Map, a set of all possible piercepoints through which a boost-through-reentry trajectory can be flown to a fixed target, contains valuable information about the …

    mit Repository record for Boost through reentry trajectory planning for maneuvering reentry vehicles (opens in a new tab)

  7. Analysis of a target defense game

    A maneuvering reentry vehicle (evader) and missile interceptor (pursuer) engagement is modeled in two dimensions, with constant velocity vehicles subject to bounded accelerations. Parameterized guidance laws are constructed for both players and a continuous, but finite-dimensional game is …

    vt Repository record for Analysis of a target defense game (opens in a new tab)

  8. Improved convergence for optimization of evasive maneuvering

    … evasive maneuvers for a Maneuvering Reentry Vehicle (MaRV) attacking a target defended with Anti-Ballistic Missiles (ABMs). The problem is large in terms of the number of optimization parameters, and perhaps in terms of the number of nonlinear constraints. Since both MaRV and ABM …

    vt Repository record for Improved convergence for optimization of evasive maneuvering (opens in a new tab)

  9. New methodologies for onboard generation of Terminal Area Energy Management trajectories for autonomous reusable launch vehicles

    … greatly increases an autonomous reusable launch vehicle's capacity for recovering from unexpected disturbances or anomalous conditions. Such capability dispenses with the routine of pre-defined, mission specific trajectories and contingencies, which has been in use since the early days of the …

    mit Repository record for New methodologies for onboard generation of Terminal Area Energy Management trajectories for autonomous reusable launch vehicles (opens in a new tab)

  10. Optimal trajectory design under uncertainty

    Reference trajectory design for atmospheric reentry vehicles can be accomplished through trajectory optimization using optimal control techniques. However, this method generally focuses on nominal vehicle performance and does not include robustness considerations during trajectory design. This …

    mit Repository record for Optimal trajectory design under uncertainty (opens in a new tab)

  11. Optimal trajectory-shaping with sensitivity and covariance techniques

    … then applied to a generic hypersonic recoverable reentry vehicle. The trajectories include uncertainties in atmospheric density, axial and normal force coefficients, commanded attitude, and initial position and velocity. Reachability footprints with uncertainty bounds are generated by the …

    mit Repository record for Optimal trajectory-shaping with sensitivity and covariance techniques (opens in a new tab)

  12. An airbag-based crew impact attenuation system for the Orion Crew Exploration Vehicle

    It is a well known fact that every capsule-shaped reentry vehicle developed by NASA was initially conceived to land on land, but was ultimately designed to land in water. In all cases, the primary factor contributing to this fundamental shift was related to difficulties with keeping the vehicle to …

    mit Repository record for An airbag-based crew impact attenuation system for the Orion Crew Exploration Vehicle (opens in a new tab)

  13. Batch-microfabricated miniaturized planar arrays of Langmuir probes for reentry plasma diagnostics and nanosatellites

    … goals in spacecraft design is maintaining the vehicle's integrity under the extreme conditions encountered during reentry to the Earth's atmosphere. When a hypersonic vehicle travels through the atmosphere, a high-density and low-temperature plasma sheath forms around it due to shock heating of …

    mit Repository record for Batch-microfabricated miniaturized planar arrays of Langmuir probes for reentry plasma diagnostics and nanosatellites (opens in a new tab)

  14. Damping Effects of Drogue Parachutes on Orion Crew Module Dynamics

    … to the CM dynamics for preliminary entry vehicle system design. More wake effects should be included to better model the system. These results are being used to improve simulation model fidelity of CM flight with drogues deployed, which has been identified by the project as key to a …

    vt Repository record for Damping Effects of Drogue Parachutes on Orion Crew Module Dynamics (opens in a new tab)

  15. Reducing turbulence- and transition-driven uncertainty in aerothermodynamic heating predictions for blunt-bodied reentry vehicles

    … those found on the NASA Orion Multi-Purpose Crew Vehicle (MPCV) thermal protection system during atmospheric reentry from the International Space Station have been studied by direct numerical simulation, with the ultimate goal of reducing aerothermodynamic heating prediction uncertainty. …

    texas Repository record for Reducing turbulence- and transition-driven uncertainty in aerothermodynamic heating predictions for blunt-bodied reentry vehicles (opens in a new tab)