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Master Thesis (m/f/d) "Conception of a smart primary power supply within aerospace application / environment"

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AES Aerospace Embedded Solutions GmbH
Munkavégzés helye

Németország

Munkaidő, foglalkoztatás jellege
- Teljes munkaidő
- Általános munkarend
Elvárások
- Angol középfok
- 1-3 év tapasztalat
- Középiskola

Állás elmentve

A hirdetést eltávolítottuk a mentett állásai közül.

Responsibilities

Objective:

The objective of the Master Thesis is to establish a concept for a future smart embedded primary power supply including applicable control and monitoring logics and validate the concept with bread board or evaluation boards.

Detailed work packages of the master thesis:

Definition of key requirements for a primary power supply regarding input voltage conditions (derived from DO-160 G regulations), secondary supply including load variations, targeted buck converter efficiency and all monitoring and protections features
Development of different smart primary power supply concepts including the definition of evaluation criteria (e.g. efficiency, weight, scalability, monitoring capability)
Validation of the most promising concept via dedicated lab demonstrators
Summary of validation activities including documentation of the most promising concepts

Applicable Standards (which will be used and experience established):

DO256 Airborne HW development standards including component management plan
DO-160G Airborne Qualification Standards

Requirements

Ongoing studies in in the field of electrical engineering or aerospace/space technic
Principle electronics design knowledge including experience in electrical circuit simulations
Knowledge regarding galvanic isolated power supply designs [e.g. flyback converter]
Experience in VHDL programming
Structured, collaborative and responsible way of working
Very good knowledge of written and spoken English (B2 level or higher)

What we offer

Attractive salary
Central location at Hirschgarten with excellent public transport connections
Flexible time management

Company info

Future aircraft electronics is being forced to reduce weight and improve failure diagnostics. The primary power supply of an electronics device might provide relevant capabilities to support weight reduction by optimizing the efficiency of a primary power supply and integrating monitoring functions within a dedicated processing unit.