This is High Altitude Aeronautical Platform Stations (HAAPS) Seminar Report made by Aeronautical, Electronics and Telecommunication Engineers and is the name of a technology for providing wireless narrow band and broad-band telecommunication services as well as broadcasting services with either airships or aircraft's.A high altitude telecommunication system comprises an airborne platform typically at high atmospheric or stratospheric altitudes – with a telecommunications payload, and associated ground station telecommunications equipment.

The High Altitude Long Operation (HALO) Network is a broadband wireless metropolitan area network (MAN) consisting of HALO aircraft operating at high altitude and carrying an airborne communications network hub and network elements on the ground.

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M.Tech Seminar Report On Sensors And Actuator System Of Special Hyper Redundant Robot

Abstract: This is a M.Tech seminar report on Sensors And Actuator System Of Special Hyper Redundant Robot and submitted to Department of Aerospace Engineering. Spatial Hyper Redundant Robot (SHR) is an all terrain robot and sometimes has special features like climbing ladder or a pole or climbing through a vertical duct, it requires special arrangement of sensors throughout its body. The whole report tells about different type of sensor, actuators, joint designing,  etc. through chapters. 

The above image shows a actuated universal joint discussed in this seminar report. In this report, the roll of sensors and actuators in SHR and their implementation in various type of design philosophy has been reviewed. Different types of joint architectures has been also discussed here and it has been found that modern researches on actuator implementation is evolved around the necessity of a perfect joint mechanism, which can give an uniform performance in versatile conditions.

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Application of Compound Compressible Flow to Hypersonic Three-Dimensional Inlets

Abstract: A method for correcting flow non-uniformities and incorporating multiple oblique shocks waves into compound compressible flow is presented. This method has several applications and is specifically presented for the problem of creating a streamline-traced hypersonic three-dimensional inlet. This method uses compound compressible flow theory to solve for the freestream flow entering a pre-defined duct with a desired downstream profile. This method allows for multiple iterations of the design space and is computational inexpensive. A method is also presented for modeling a laminar or turbulent boundary layer to compare inlet designs and to determine the viscous correction to the inlet. Two different Mach 6 designs were evaluated, with a rectangular capture area and circular combustor with a uniform temperature, pressure, and Mach number profile. Comparison with other three-dimensional inlets indicates those designed with this method demonstrate good inviscid performance. These inlets also have the ability to correct incoming flow non-uniformities.

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