A Low Cost Portable Telemetry and Telecommand Station For The Brazilian

Data Collecting Satellites

 

Mário Eugênio Saturno       Carlos Eduardo Santana       Jânio Kono

            saturno@dea.inpe.br                santana@dss.inpe.br         kono@dss.inpe.br

National Space Research Institute (INPE)

São José dos Campos - SP - Brazil

Phone: 55-123-25-6186, Fax: 55-123-25-6225

 

Abstract

The first Data Collecting Satellite Brazilian, developed by the National Space Research Institute (INPE), has completed three and half years of successful operation in orbit. The launching characteristics required INPE to develop a Portable Telemetry and Telecommand Station (TTS). The hardware developed is distributed in two boards installed in an IBM-PC compatible computer. The TTS can also retransmit telemetry data to another station through a common telephone line and a pair of modems. The TTS software was designed so that system reconfiguration is done easily using a text editor and was implemented very fast, in four months, mainly due to the use of Pascal language and reuse of existing modules. Besides all the Satellite Functional tests done in the launch Campaign, the TTS was also used to control the satellite during the first three orbits. This success encouraged INPE to develop a new TTS based on DSP technology and notebook computer.

 

 

1 - Introduction

 

The Brazilian National Space Research Institute (INPE) developed the first Data Collecting Satellite (SCD-1). The SCD-1 is a low earth orbit spin stabilized satellite, 25 degree inclination and 750 km altitude. It is a dedicated satellite to the collection of environmental data emitted by Data Collecting Platform (DCP) distributed over Brazilian territory. The DCP is small automatic, unattended earth station which collects weather and other local environment data for transmission to satellite in short intermittent bursts[1].

The SCD-1 Service Telecommunication (TMTC) and On-Board Supervision subsystems are composed by S-band antennas, transponder, TC decoder, TM encoder and an On-Board Computer. The TM and TC frames follows the ESA format [2,3]. The SCD-1, launched by the Pegasus launcher at February 9, 1993, has completed three and half years of successful operation in orbit. The next satellite, the SCD‑2 is similar to the first, it is ready and a launcher is being procured.

During the SCD-1 Assembling, Integration and Testing activities, a conventional check-out system based on HP‑1000 minicomputer, a telemetry receiver and a telecommand generator equipment was used. This type of check-out system is heavy, big, complex, and needs air-conditioning. The launching characteristics of Pegasus required SCD-1 check-out tests to be performed in several and adverse conditions, including at the airport runway before the launch with the launcher integrated in the aircraft. This requirements includes portability, simplicity, use of an IBM-PC compatible computer, high level language, software reconfiguration facilities.

 

 

2 - Portable Telemetry and Telecommand Station general requirements

 

INPE had to develop a Portable Telemetry and Telecommand Station (TTS) to support all the Satellite Functional tests done in the launch Campaign. The TTS requirements are:

1)   be portable;

2)   distribute the hardware in ISA boards;

3)   use an IBM-PC like as platform;

4)   receive and store telemetry;

5)   visualize telemetry in real time;

6)   export telemetry data to a file;

7)   display TM parameters out-of-limits;

8)   transmit On/Off and On-Board Computer telecommands and make a log;

9)   retransmit TM to a remote station through phone line;

10)    and reconfigurate using a text editor: telemetry screens, calibration curves, telecommand sequences.

 

 

3 - System description

 

INPE had already developed a test equipment to test the On-Board Computer based on an IBM‑PC compatible computer. The hardware could send NRZ‑L telecommands and receive PSK modulated telemetries[4]. The TTS was upgraded to send PSK modulated telecommands. The software already developed comprises of receive and store TM and send TC. The TTS software was upgraded to monitor real time TM requiring a good user interface. Figure 1 shows the TTS.

 

 

TC Video (PSK)           

                       Umbilical

TM Video (PSK)

 

 

 
                                            

  

Figure 1 - TTS

 

 

3.1 - TTS Hardware

 

The Portable Telemetry and Telecommand Station was developed using an IBM‑PC compatible computer as platform. The hardware developed to send telecommands and receive telemetries is distributed in two boards. The TC bit rate is 2000 bit/s, the modulation is BPSK, the code is NRZ-L, ouput level from 0.5 to 8.0 Vp (adjustable) and impedance 50 W. The TM bit rate is 2048 bit/s, the modulation is BPSK, the code is Bi-phase-L, input level from 0.5 to 5.0 Vp and impedance 50 W.

The telecommand generator is composed of an NRZ data encoder and a PSK modulator. The Telemetry Receiver is composed of a Bi-Phase decoder, PSK demodulator, and a bit synchronizer. Figure 2 presents the TTS Hardware Block Diagram. The TM reception is implemented using interruption.


 



       NRZ-L         Bi-Phase       P S K   TM 

       Decoder       Decoder      Demodulat video

                                 

   PC                                  Umbilical

       NRZ-L          P S K             TC     

  Bus Encoder         Modulator          Video

 


Figure 2 - TTS Hardware Block Diagram

 

 

3.2 - Portable Telemetry and Telecommand Station Software

 

The TTS software was divided into modules: TM acquisition, TM storage, TM presentation, TC transmission and logging, reusing existing and tested modules, and it was programmed using Turbo Pascal 6.0, a high-level structured programming language with a good debugger. The prototype model was used to develop user interface and it was very useful to create a model of the TTS Software. This was responsible for the very fast development of the software, in four months. Figure 3 shows the TTS Software main modules and its interfaces.

A text editor can easily change the telemetry calibration curves, graphic or text type screens and the parameters shown in each screen, the telecommands and the software operation mode. These features are important to allow fast reconfiguration of the TTS for different mission phases and equipment. The figure 4 presents a graphic screen.

 

 

 

 

 

 

 


TM

Present

 
                                                           

 

 

 

 

 


                                                                                     

 

 

Figure 3 - TTS Software Architeture

 

Figure 4 - Graphic screen

 

 

4 - Conclusions

 

The TTS hardware was tested using an osciloscope and satellite integration model. The software was tested following the exhaustive input testing (Black-Box model). The telecommands and telemetry parameters were verified by an expert. After that, it was used during the SCD-1 Assembling Integration and Testing activities.

The TTS was used with success during the launching campaign tests and it was used receive telemetries and control the satellite during the first three orbits from Alcântara Launching Center (CLA), in Maranhão state, near the equator line.

This success, in special a good performance and low cost of the equipment, encourages INPE to develop a new TTS based on DSP technology (TMS 320C25) and notebook computer to be used during the launching campaign tests for the SCD‑2.

 

 

5 - References

 

1.        J. Kono, C.E. Santana: "SCD1: One Year In Orbit", Proceedings of International Symposium on Spacecraft Ground Control and Flight Dynamics, 7-11 February 1994, São José dos Campos, Brazil.

2.        ESA, PCM Telecommand Standard, ESA-PSS-45 (TTC-A-01), 1978.

3.        ESA, PCM Telemetry Standard, ESA-PSS-46 (TTC-A-02), 1978.

4.        M.E. Saturno, J.D.D. Alonso, J.C. Caliman: "On-board computer data handling testing experiences for the second Brazilian data collecting satellite (SCD-2)", International Conference on Small Satellites: Missions and Technology, 9-13 september 1996, Madri, Espanha.

 

   

 

 

 


Dr. Bernd Kirchner

 

DLR, Institute of Space Sensor Technology

 

Subj.: Paper IAA-B01003

 

Rudower Chaussee 5

 

D-12484 Berlin

 

Germany

 

 

 

 

 

 

 

Mário Eugênio Saturno

Divisão de Eletrônica Aeroespacial

Instituto Nacional de Pesquisas Espacial

Av. dos Astronautas, 1758 - Jardim da Granja

12227-010  São José dos Campos -  SP - Brasil