The Following Are some of the Seminar Topics and Project Titles For Aerospace Engineering:

1. Re-Entry Of Space
2. Vehicle Ramjet, Scramjet Engines
3. Aircraft navigation Systems 
4. Space Shuttles And Its Advancements 
5. Advances  in Rocket Propulsion 
6. Quasi Turbine Engines 
7. Low Cost Spacecraft Simulator 
8. Clearance of Space Debris 
9. Materials used in Space Re-entry Vehicles 
10. Fuel Cells on Aerospace 
11. Advanced flight technology 
12. Magnetoplasmadynamic thruster 
13. Advanced Space Vision System 
14. Aeroelasticity 
15. Lithobraking 
16. Lunar space elevator 
17. Fixed-wing aircraft 
18. Space transport 
19. Hohmann transfer orbit 
20. Early Flying machines 
21. Sigma Gamma Tau (aerospace engineering honor society) 
22. Electrotechnology 
23. Gas-generator cycle (rocket) 
24. Antimatter rocket 
25. Apsis HyShot 
26. Atmospheric reentry issues 
27. Avionics 
28. Kessler Syndrome 
29. Relativistic rocket 
30. Nose cone design 
31. Redshift rocket 
32. Big dumb booster 
33. Ablative laser propulsion
34. High Altitude Technology 
35. Safety in aerospace engineering 
36. Landing and take-off of aerospace vehicles. 
37. Advanced Fuels in aerospace engineering 
38. Control system used in aerospace vehicles

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Title: Categorizing Admittance Control Parameters for the Ranger 8-DOF Tele-operated Space Manipulator
Abstract: Position-based admittance control of a robotic manipulator is a strategy that allows the manipulator to achieve compliance without sacrificing positional accuracy or modifying the underlying position controller. Desired manipulator stiffness and damping can be specified so that the tool tip behaves as a spring-dashpot system. This work characterizes the range of parameters that allows stable task execution in contact with an environment of varying stiffness for the Ranger dexterous manipulator. A classical stability analysis and simulation of the controller is conducted to predict its response in contact. The manipulator's behavior is then observed during a series of simple tasks involving contact in one and two degrees of freedom. Suitable gains are chosen such that interaction forces at the tool tip are kept low. A compliant peg-in-hole insertion task is successfully accomplished. The work also outlines the implementation of an algorithm that removes unwanted gravity forces measured at the tool tip.

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Keywords: Engineering, Aerospace, Impedance, Admittance, Control, Robotic Manipulator
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Autonomous Target Recognition and Localization for Manipulator Sampling Tasks

This is a Aeronautical Engineering Theses

Abstract on Project: Future exploration missions will require autonomous robotic operations to minimize overhead on human operators. Autonomous manipulation in unknown environments requires target identification and tracking from initial discovery through grasp and stow sequences. Even with a supervisor in the loop, automating target identification and localization processes significantly lowers operator workload and data throughput requirements. This thesis introduces the Autonomous Vision Application for Target Acquisition and Ranging (AVATAR), a software system capable of recognizing appropriate targets and determining their locations for manipulator retrieval tasks.

AVATAR utilizes an RGB color filter to segment possible sampling or tracking targets, applies geometric-based matching constraints, and performs stereo triangulation to determine absolute 3-D target position. Neutral buoyancy and 1-G tests verify AVATAR capabilities over a diverse matrix of targets and visual environments as well as camera and manipulator configurations. AVATAR repeatably and reliably recognizes targets and provides real-time position data sufficiently accurate for autonomous sampling.

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Keywords: Engineering, Aerospace

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This is a Aerospace Project On Bending Of Selectively Reinforced Beams is good project report and experiment for students which aims to investigate the flexural behavior of structural beam elements through experimentation and analysis. Additionally, the goal of the experiment is to assess the utility of composite materials as reinforcement components. In this 3 beams will be tested viz. an aluminum beam, an aluminum with aluminum caps, and an aluminum with graphite/epoxy caps.The beam with the thin aluminum top and bottom pieces will theoretically deflect more than the beam with the extra aluminum caps.

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