ATB – AOCS Test Bed Simulation Framework

ATB is a software simulation framework modelling orbital and spacecraft dynamics, environment, and AOCS sensors and actuators. It is an ideal tool for organisations wanting to increase their awareness and knowledge of satellite AOCS closed loop systems. It includes closed-loop functional control models which utilise the sensor and actuator software models, and is an excellent starting point for system concept analysis, and attitude and orbit control algorithm development.

The ATB contains the following features:

 

  • The SIMSAT simulation environment in windows operating system, providing test script capability, Graphical User Interface (GUI) and the generic models for orbit and environment (PEM) and dynamics (SIMDYN)
  • An AOCS Functional Control Model providing simple AOCS control algorithm for communication with the sensors and actuators
  • A set of actuator models including: Reaction Wheel, Magnetotorquer, and Propulsion System
  • A set of sensor models including: Sun Sensor, Star Tracker, GPS, Gyro, and Magnetometer
  • Strong heritage and quality in simulation
    environment.

 

ATB is based on the simulation infrastructure SIMSAT used by the European Space Agency (ESA) for all mission preparation and operations.

 

SIMSAT provides the environment for real-time or faster-than-real-time simulation. It provides the following facilities:

 

  • Simulation model tree including model data and services
  • Alpha-numeric and graphical displays, data recording
  • Real-time scheduling and scheduler display
  • Logging
  • JavaScript engine for running simulator command sequences and test scripts

 

Efficient method to develop knowledge in AOCS systems and Attitude/Orbit Control

ATB offers a cost-efficient and risk-adverse solution to organisations starting development of AOCS systems and Attitude and Orbit Control Software. The system provides template models for typical Earth Observation sensors and actuators, and also a functional control model handling the closed-loop control of the system. The closed-loop control includes algorithms for the following modes of operation:

 

  • De-tumbling, Sun Acquisition, Course and Fine Attitude Control, Momentum Dumping and Orbital Correction

 

ATB has been designed to allow users to quickly and simply install and set-up the system. This means that closed loop control simulation can be executed immediately when the ATB is installed.

 

The user can use the initial template models to learn about the systems and then configure, customise, modify, or replace the model algorithms with their own refinements. ATB can then be used to test the algorithms in a closed-loop real-time (or faster than real-time) simulation.

 

Potential to expand simulation to full operational simulator

ATB provides an excellent platform to develop a full operational simulator to support satellite programmes. A full operational simulator includes software models for all satellite systems and interfaces to the ground system for command and control. A full satellite simulator provides numerous benefits to the satellite programme, including:

 

  • Verification and Validation of ground segment systems
  • Verification and Validation of operational concepts and procedures
  • Training of operations engineers
  • Reduces performance risk of programme through effective means of operations preparation
  • Low-cost, flexible and tailorable approach

 

Contact VEGA about the ATB – AOCS Test Bed Simulation Framework