Table of Contents
Aeronautical engineering project topics for the final year
| S.No. | Projects | Abstract |
|---|---|---|
| 1. | Design of sliding mode flight control system for a flexible aircraft. The design of a sliding mode flight control system for a flexible aircraft involves implementing a robust control strategy that dynamically adjusts to the aircraft’s varying structural dynamics, ensuring stability and performance by employing a sliding surface to drive the system towards optimal states despite uncertainties and disturbances. Get help | Abstract |
| 2. | Nonlinear Filter and Neural Modeling for Calibration of Aircraft Airdata System. Nonlinear filters and neural modeling are employed synergistically for the calibration of aircraft airdata systems, enhancing accuracy and reliability in capturing complex, nonlinear relationships within the data, thereby improving the overall performance and safety of flight instrumentation. Get help | Abstract |
| 3. | Lateral Directional Aircraft Aerodynamic Parameter Estimation Using Adaptive Stochastic Nonlinear Filter The Lateral Directional Aircraft Aerodynamic Parameter Estimation Using Adaptive Stochastic Nonlinear Filter is a sophisticated method that employs advanced stochastic nonlinear filtering techniques to accurately estimate the aerodynamic parameters governing the lateral and directional behavior of an aircraft, enhancing flight control system performance and overall aviation safety. Get help | Abstract |
| 4. | Aircraft Neural Modeling and Aerodynamics Parameter Estimation using Neural Partial Differentiation Aircraft Neural Modeling and Aerodynamics Parameter Estimation using Neural Partial Differentiation involves employing neural networks to model the complex aerodynamics of aircraft, enabling accurate estimation of key parameters through the utilization of neural partial differentiation techniques. This innovative approach enhances understanding and optimization of aircraft performance. Get help | Abstract |
| 5. | System Identification of Flexible Aircraft in Frequency DomainSystem Identification of Flexible Aircraft in the Frequency Domain involves analyzing the dynamic behavior of an aircraft by characterizing its response to various input frequencies, enabling precise modeling and control strategies for optimal performance in diverse flight conditions. Get help | Abstract |
| 6. | Stochastic Contraction Based Online Estimation of Second Order Wiener System Stochastic Contraction-Based Online Estimation of Second Order Wiener System is a mathematical approach that utilizes stochastic contraction theory for real-time estimation of parameters in second-order Wiener systems, enhancing accuracy in modeling dynamic nonlinear processes. Get help | Abstract |
| 7. | Stochastic Contraction Based Observer and Controller Design Algorithm with Application to a Flight Vehicle The Stochastic Contraction Based Observer and Controller Design Algorithm is a methodology employed in control systems, particularly for flight vehicles, utilizing stochastic contraction theory to enhance stability and performance in uncertain environments by designing observers and controllers. This algorithm is tailored to address the challenges of ensuring robustness and reliability in aerospace applications. Get help | Abstract |
| 8. | Design and Convergence Analysis of Stochastic Frequency Estimator using Contraction TheoryThe Design and Convergence Analysis of Stochastic Frequency Estimator using Contraction Theory involves developing a method to estimate frequencies in stochastic signals, utilizing Contraction Theory to ensure the convergence and stability of the estimator, enhancing its reliability in dynamic and uncertain environments. Get help | Abstract |
| 9. | Multi-sensor Data Fusion based Approach for the Calibration of Airdata System The Multi-sensor Data Fusion approach for Airdata System Calibration integrates data from diverse sensors, such as inertial measurement units and air pressure sensors, enhancing accuracy and reliability in measuring aircraft parameters like altitude and airspeed. This method ensures robust calibration by synthesizing information from multiple sources, optimizing overall system performance. Get help | Abstract |
| 10. | Reduced Order Model based Flight Control System For A Flexible Aircraft The Reduced Order Model based Flight Control System for a Flexible Aircraft utilizes simplified mathematical representations to efficiently manage and stabilize the aircraft’s flexible structures, enhancing control precision and reducing computational complexity in comparison to traditional models. Get help | Abstract |
| 11. | Contraction Based Tracking Control of Autonomous Underwater VehicleContraction-based tracking control for Autonomous Underwater Vehicles (AUVs) involves utilizing contraction theory to design control strategies that ensure stable and accurate tracking of desired trajectories, enhancing the navigation and performance of underwater autonomous systems. Get help | Abstract |
| 12. | Lateral-Directional Aerodynamics Parameter Estimation using Neural Partial Differentiation The Lateral-Directional Aerodynamics Parameter Estimation using Neural Partial Differentiation involves utilizing neural networks to compute partial derivatives, enhancing the accuracy of estimating aircraft aerodynamic parameters related to lateral and directional stability. Get help | Abstract |
