There are three modules offered in this short course. The short course fee is listed below.
| Fees | International | Local |
| IEEE Member | USD 250 | RM 750 |
| Non-IEEE Member | USD 300 | RM 900 |
Module 1: Optical Payload Design for Near Equatorial Satellite
1. Course Overview
Optical Payload Design Training is essential for every engineer who designs the optical payload. In order to strengthen the design experiences and skills in Optical Payload System, ATSB® is pleased to offer the optical payload design training emphasizing on the Near Equatorial Satellite for customers.
2. Course Objectives
The objective of the training program is to give participants a background and solid knowledge in optical payload design.
3. Course Outcomes
Participants shall be able to perform basic design of optical payload for Near Equatorial Satellite.
4. Pre-requisites and Target Participants
Engineering, Mathematics or Physics background. Entry level and professionals.
1. Course Overview
Power budget is part of the System Engineering of satellite and is used as the baseline in designing Satellite Power Subsystem. A specific method is used to calculate the power budget for specific orbit i.e. Near Equatorial Orbit (NEqO), Sun-Synchronous and GEO.
This training will cover on fundamental of satellite power subsystem and how to design power budget for Near Equatorial satellite.
2. Course Objectives
The objective of the training program is to give participants a background and solid knowledge in Power Budget for Near Equatorial Satellite.
3. Course Outcomes
Participants shall be able to select power subsystem design and perform power budget in satellite development especially for satellite orbiting in Near Equatorial.
4. Pre-requisites and Target Participants
Engineering, Mathematics or Physics background. Entry level and professionals.
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Module 3:
Launch Opportunity for Piggyback Satellites to Near Equatorial Orbit (NEqO) and Introduction to Orbital Simulation
1. Course Overview
In this section, participants will be exposed to the overview of the launch systems, the basic of the launch vehicle considerations and the launch systems selection process.
Participants will be exposed to the important considerations in launching any satellites and confirm all of the mechanical and electrical interfaces are compatible with the selected launch vehicle.
Participants will be exposed to the planning of launching a primary satellite with the secondary satellites.
In addition, participants will be shown how orbits are simulated using orbital simulation software and how Orbital Insertion is analysed.
2. Course Objectives
The objective of the training program is to give participants a background and solid knowledge in preparing for piggyback launch opportunity and orbital simulation.
3. Course Outcomes
Participants shall be able to select the suitable launch system for piggyback satellites to Low Earth Orbit (LEO) mission and to outline the necessary electrical and mechanical interfaces. Participants shall be able to understand the use of simulation software as a tool for orbit simulation and design use.
4. Pre-requisites and Target Participants
Engineering, Mathematics or Physics background. Entry level and professionals.
