Atmel AT7910E Manuale utente

AT7910E

SpW-10X SpaceWire Router

DATASHEET

Features

SpaceWire Router

Logical to Physical addressing translation

Priority Management

Header Deletion Capability

Eight Bidirectional SpaceWire links

Full duplex communication

Data rate from 2 up to 200 Mbit/s in each direction

Two External Interfaces

Dedicated Input and Output FIFOs

9-bit wide Interface

Configuration Port

Read/Write Accesses to internal registers

Accessible from both the spacewire links (8 channels) and the external interfaces

Remote Memory Access Protocol (RMAP) support

Time Code Interface

Master/Slave Capability

Error/Status Interface

Operating range

Voltages 3V to 3.6V

Temperature - 55°C to +125°C

Maximum Power consumption

All spacewire links active at 200Mbit/s : 4W

Radiation Performance

Total dose tested successfully up to 300 Krad (Si)

No single event latchup below a LET of 80 MeV/mg/cm2

ESD better than 2000V

Quality Grades

QML-Q or V with SMD

Package: 196pins MQFPF

Mass: 12grams

7796G AERO 02/13

AT7910E [DATASHEET]

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Description

The SpW-10X SpaceWire routing switch is capable of connecting many nodes, providing

a means of routing packets between the nodes connected to it. It comprises eight

SpaceWire link interfaces and a routing matrix. The routing matrix enables packets

arriving at one link interface to be transferred to and sent out of another link interface on

the routing switch.

The AT7910E was designed by Austrian Aerospace (Austria) and the University of

Dundee (Scotland). It is manufactured using the SEU hardened cell library from Atmel

MH1RT CMOS 0.35µm radiation hardened sea of gates technology.

For any technical question relative to the functionality of the AT7910E please contact

Atmel technical support at [email protected].

This document must be read in conjunction with the University of Dundee “SpaceWire

Router SpW-10X User Manual” available at www.atmel.com.

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Table of Contents

1. Functional Description........................................................................4

1.1 SpaceWire Ports...............................................................................................5

1.2 External Ports....................................................................................................5

1.3 Configuration Port.............................................................................................5

1.4 Routing table.....................................................................................................5

1.5 Routing control logic and crossbar....................................................................6

1.6 Time Code Processing......................................................................................6

1.7 Control/Status Registers...................................................................................6

2. Typical Applications ...........................................................................7

2.1 Stand-alone router ............................................................................................7

2.2 Node interface...................................................................................................7

2.3 Embedded router ..............................................................................................8

3. PLL Filter ...........................................................................................9

4. LVDS Interface.................................................................................10

4.2 AT7910E Limitation.........................................................................................10

4.3 AT7910E Compatibility with LVDS receiver Standards...................................11

5. Package Information........................................................................12

5.1 Package Outline..............................................................................................12

5.1.1 MQFPF 196......................................................................................12

5.2 Pin Description................................................................................................14

5.3 Electrical Characteristics.................................................................................16

5.4 Absolute Maximum Ratings ............................................................................16

5.5 DC Electrical Characteristics...........................................................................16

5.6 Power consumption.........................................................................................16

5.7 AC Electrical Characteristics...........................................................................17

6. Ordering Information........................................................................19

6.1 AT7910E Ordering Codes...............................................................................19

7. Revision History...............................................................................20

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1. Functional Description

The SpaceWire router comprises the following functional logic blocks:

Eight SpaceWire bi-directional serial ports.

Two external parallel input/output ports each comprising an input FIFO and an output FIFO.

A non-blocking crossbar switch connecting any input port to any output port.

An internal configuration port accessible via the crossbar switch from the external parallel input/output port or the

SpaceWire input/output ports.

A routing table accessible via the configuration port which holds the logical address to output port mapping.

Control logic to control the operation of the switch, performing arbitration and group adaptive routing.

Control registers than can be written and read by the configuration port and which hold control information e.g. link

operating speed.

An external time-code interface comprising tick_in, tick_out and current tick count value

Internal status/error registers accessible via the configuration port

External status/error signals

A block diagram of the routing switch is given in the following figure:

Figure 1. SpaceWire Router Block Diagram

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The AT7910E provides a routing capability between eight SpaceWire links according to the SpaceWire Standard ECSS-

E-50-12A. In addition for use as a node interface, the AT7910E integrates other interfaces such as:

External ports

Configuration port

Time-code interface

Control/Status interface

1.1 SpaceWire Ports

The SpaceWire router has eight bi-directional SpaceWire links each compliant with the SpaceWire standard ECSS-E-50-

12A.

Each SpaceWire link is controlled by an associated link register and routing control logic. Packets received on SpaceWire

links are routed by the routing control logic to the configuration port, other SpaceWire link ports or the external FIFO ports

depending on the packet address.

Packets with invalid addresses are discarded by the SpaceWire router. The SpaceWire link status is recorded in the

associated link register and error status is held by the router until cleared by a configuration command.

1.2 External Ports

The SpaceWire router has two bi-directional parallel FIFO interfaces that can be used to connect the router to an external

host system. The external port FIFO is two data characters deep.

Each FIFO is written to or read from synchronously with the 30MHz system clock.

An eight-bit data interface and an extra control bit for end of packet markers are provided by each external port FIFO.

Packets received by the external port are routed by the routing control logic to the configuration port, SpaceWire link ports

or the other external port depending on the packet address.

Packets with invalid addresses are discarded by the SpaceWire router.

1.3 Configuration Port

The SpaceWire router has one configuration port which performs read and write operations to internal router registers.

Packets are routed to the configuration port when a packet with a leading address byte equal to zero is received. The

Remote Memory Access Protocol (RMAP) is used to access the configuration port.

If an invalid command packet is received then the error is flagged to an associated status register and the packet is

discarded.

1.4 Routing table

The SpaceWire router routing table is set by the router command packets to assign logical addresses to physical

destination ports on the router.

A group of destination ports can be set, in each routing table location, to enable group adaptive routing. When a packet is

received with a logical address the routing table is checked by the routing control logic and the packet is routed to the

destination port when the port is ready. Routing table locations are set to invalid at power on or at reset.

The routing table logical addresses can also be set to support high priority and header deletion. High priority packets are

routed before low priority packets and header deletion of logical addresses can be used to support regional logical

addressing.

An invalid routing address will cause the packet to be spilled by the control logic.

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1.5 Routing control logic and crossbar

The routing control logic is responsible for arbitration of output ports, group adaptive routing and the crossbar switching.

Arbitration is performed when two or more source ports are requesting to use the same destination port.

A priority based arbitration scheme with two priority levels, high and low, is used where high priority packets are routed

before low priority packets. Fair arbitration is performed on packets which have the same priority levels to ensure each

packet gets equal access to the output port.

Group adaptive routing control selects one of a number of output ports for sending out the source packet.

1.6 Time Code Processing

An internal time-code register is used in the router to allow the router to be a time-code master or a time-code slave.

In master mode the time-code interface is used to provide a tick-in to the SpaceWire routing causing time-codes to be

propagated through the network. Two modes of time master operation are supported, an automatic mode where a time-

code is propagated on each external tick-in and a normal mode where the time-code is propagated dependent on the

external time-in signal.

In time-code slave mode a valid received time-code, one plus the value of the router time-code register, causes a tick-out

to be sent to the SpaceWire links and the external time-code interface. The time-code is propagated to all time-code ports

except the port on which the time-code was received. If the time-code received is not one plus the value of the time-code

register then the time-code register is updated but the tick-out is not performed. In this way, circular network paths do not

cause a constant stream of time-codes to be sent in a loop.

1.7 Control/Status Registers

The control and status registers in the SpaceWire router provide the means to control the operation of the router, set the

router configuration and parameters or monitor the status of the device. The registers are accessed using RMAP

command packets received by the configuration port.

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2. Typical Applications

The AT7910E SpaceWire router is perfectly suited for development of applications requiring a standalone router, a

terminal node with SpaceWire interface or a mixed configuration of the two previous ones.

2.1 Stand-alone router

The AT7910E SpaceWire Router may be used as a stand-alone router with up to eight SpaceWire links connected to it.

Configuration of the routing tables etc. may be done by sending SpaceWire packets containing configuration commands

to the router.

Figure 2-1. AT7910E as SpaceWire router

2.2 Node interface

The SpaceWire Router has two external ports which enable the device to be used as a node interface. The equipment to

be connected to the SpaceWire network is attached to one or both external ports. One or more SpaceWire ports are used

to provide the connection into the SpaceWire network. Unused SpaceWire ports may be disabled and their outputs tri-

stated to save power. In this arrangement configuration of the routing tables and other parameters may be done by

sending configuration packets from the local host via an external port or from a remote network manager via a SpaceWire

port.

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Figure 2-2. AT7910E as SpaceWire node interface

2.3 Embedded router

The SpaceWire Router device can also be used to provide a node with an embedded router. In this case the external

ports are used to provide the local connections to the node and the SpaceWire ports are used to make connections to

other ports in the network.

Figure 2-3. AT7910E as Embedded Router

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3. PLL Filter

The AT7910E uses an internal PLL to provide the base transmit clock signal for the SpaceWire interfaces. External

components are required to implement the PLL loop filter and to provide a bias for the PLL VCO.

Note that RVCO, C and C0 are all connected to a quiet common ground track.

Dedicated decoupling capacitors are also required for the PLL power supply.

Figure 3-1. PLL filter and decoupling capacitors

Table 3-1. PLL filter recommended components

Component

Value

10kW ± 5%, ¼W

120pF, ± 5%

3.3pF, ± 5%

RVCO

4.7kW for 100-150MHz operation

1.8kW for 150-200MHz operation

Table 3-2. PLL decoupling capacitors

Component

Value

Cpll1

100nF, ± 5%

Cpll2

10µF, ± 5%

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4. LVDS Interface

The AT7910E provides 8 SpaceWire link based on LVDS IOs that should comply with the EIA-644 standard

requirements.

The basic LVDS interface consists in a single differential link interconnected between a transmiter and a receiver.

Such a link requires a termination resistor on the receiver side to allow high frequency transfer usage. The nominal

resistor value for the termination resistor 100 ohms. LVDS bidirectional communication principle

Figure 4-1. LVDS interface principle

Caution: The AT7910E doesn’t embed the termination resistors on the receivers.

4.1 AT7910E Limitation

Due to MH1RT technology limitation, the electrical parameters of the EIA-644 standard can not all be met on the

transmitters of the AT7910E

Figure 4-2. Output electrical characteristics

Table 4-1. AT7910E LVDS TX feature

Parameter

TIA/EIA

Standard

AT7910E

Unit

VOS min

1125

800

VOS max

1375

1568

VOD Min

247

VOD Max

454

550

DeltaVOD

DeltaVOS

(dynamic)

150

200

Voh

Vol

Vod

Gnd

Vos

Indice

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