Hartley, EN and Maciejowski, JM (2013) Predictive control for spacecraft rendezvous in an elliptical orbit using an FPGA. 2013 European Control Conference, ECC 2013. pp. 1359-1364.Full text not available from this repository.
A field programmable gate array (FPGA)-based predictive controller for a spacecraft rendezvous manoeuvre is presented. A linear time varying prediction model is used to accommodate elliptical orbits, and a variable prediction horizon is used to facilitate finite time completion of manoeuvres. The resulting constrained optimisation problems are solved using a primal dual interior point algorithm. The majority of the computational demand is in solving a set of linear equations at each iteration of this algorithm. To accelerate this operation, a custom circuit is implemented, using a combination of Mathworks HDL Coder and Xilinx System Generator for DSP, and used as a peripheral to a MicroBlaze soft core processor. The system is demonstrated in closed loop by linking the FPGA with a simulation of the plant dynamics running in Simulink on a PC, using Ethernet. © 2013 EUCA.
|Divisions:||Div F > Control|
|Depositing User:||Unnamed user with email email@example.com|
|Date Deposited:||15 Dec 2015 13:10|
|Last Modified:||14 Feb 2016 01:00|