Global ETD Search

Search theses and dissertations gathered from participating repositories worldwide. Every result links back to the library that holds it. No account is needed.

Results

Showing 1 to 10 of 10 for “"aircraft simulation"”.

  1. Aircraft simulation validation using an instrumental variable approach

    … developed which offers the potential to validate aircraft simulation models using noisy flight test measurements. The proposed validation procedure is based on the instrumental variable parameter identification method. The instrumental variable method requires a choice of "instruments." For this …

    vt Repository record for Aircraft simulation validation using an instrumental variable approach (opens in a new tab)

  2. Pseudo-linear indentification and its application to adaptive control

    … in the stochastic case are investigated through simulation and comparisons with popular methods are made. The method is then extended to allow the tracking of time-varying system parameters. An adaptive control structure based upon this Tracking–PLID algorithm is proposed which utilizes …

    vt Repository record for Pseudo-linear indentification and its application to adaptive control (opens in a new tab)

  3. Modeling and Simulation of Autonomous Thermal Soaring with Horizon Simulation Framework

    … Most research involved some form of flight simulation. Improvements to the aircraft and thermal models for simulation purpose would enable researchers to better design their UAVs and explore any potential flaws in their designs. An aircraft simulation with a thermal environment was created …

    calpoly Repository record for Modeling and Simulation of Autonomous Thermal Soaring with Horizon Simulation Framework (opens in a new tab)

  4. Hierarchical power management in vehicle systems

    … vehicle systems such as commercial and military aircraft, on- and off-road vehicles, and ships present a unique control challenge, where maximizing performance requires optimizing the generation, storage, distribution, and utilization of energy throughout the entire system and over the duration …

    uiuc Repository record for Hierarchical power management in vehicle systems (opens in a new tab)

  5. Mission-Integrated Synthesis/Design Optimization of Aerospace Subsystems under Transient Conditions

    … the thermodynamic behavior of a military aircraft have been implemented by the Air Force Research Lab (AFRL) and other Integrated Vehicle Energy Technology Demonstration (INVENT) contributors into a cohesive, adaptable, dynamic aircraft simulation program in Mathworks' Simulink®. The …

    vt Repository record for Mission-Integrated Synthesis/Design Optimization of Aerospace Subsystems under Transient Conditions (opens in a new tab)

  6. Estimation and fault diagnosis for vehicle energy systems

    … thermal management system of an electrified aircraft. Closed-loop simulation and experimental results confirm a reduction in computational cost compared to a conventional centralized observer and an increase in estimation accuracy compared to a decentralized observer which ignores coupling …

    uiuc Repository record for Estimation and fault diagnosis for vehicle energy systems (opens in a new tab)

  7. Adaptive control design with guaranteed margins for nonlinear plants

    … dynamics based on the NASA X-15 hypersonic aircraft. Simulation results show that the augmented adaptive control is able to stabilize the plant and tracks desired trajectories with uncertainties in the plant while instability cannot be overcome only with the nominal controller. The …

    mit Repository record for Adaptive control design with guaranteed margins for nonlinear plants (opens in a new tab)

  8. Methodology for the validation of aircraft simulations in a mission scenario through the use of a validation tree with uncertainty

    … uses probabilistic analysis and computational simulation to continually update the state of a fleet of aircraft. This methodology describes a process in which the aircraft that is most likely to successfully complete a mission is determined computationally, and after the mission, computational …

    uiuc Repository record for Methodology for the validation of aircraft simulations in a mission scenario through the use of a validation tree with uncertainty (opens in a new tab)

  9. Fighter Aircraft Synthesis/Design Optimization

    … 19 mission segments of a supersonic fighter aircraft mission and the results of the study show that for very large structural weight penalties and fuel penalties applied to account for the morphing technology, the morphing-wing aircraft can significantly outperform a fixed-wing AAF …

    vt Repository record for Fighter Aircraft Synthesis/Design Optimization (opens in a new tab)

  10. Modeling hybrid-electric regional jet aircraft performance & emissions reduction potential

    Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2023-04-12 without embargo terms

    uiuc Repository record for Modeling hybrid-electric regional jet aircraft performance & emissions reduction potential (opens in a new tab)