John Collins
En-Route
I thought the whole idea of NextGen was to move away from radar surveillance all to together.
Anyone know what the expected accuracy is of the required TSO'd WAAS GPS source for the average GA aircraft?
John, thanks for the email to check Out performance.
It does not look like there is enough interest in doing ADSB in a sensible way. It's a good idea but poor execution can kill even the best ideas. I think I will just go any GPS source into a Mode S-ES for now to get the ground to send traffic (ala Dynon's current solution) and do like everyone else and wait till just before 2020 to use a proper GPS source. If the FAA is going to make this hard, I'll just pass on playing.
Radar is still an integral portion of the system and is not going away. The radar is the backup when the GPS system is OOS or an aircraft has an equipment failure. It also provides protection against spoofing a position.
When the system is working, which should be a very high percentage of the time and the norm, aircraft will be able to be kept closer to each other with greater flow. When it fails, the reversion back to radar spacing will occur with the lower positional accuracy. The system will also provide coverage in some areas that now do not have radar coverage, for example over the Gulf of Mexico and in mountainous areas. It will also enable some applications such as enhanced self separation and spacing in route, IOW you can be given a clearance to follow a target that you can't see visually but know their position and your aircraft is equipped with the tools to alert on a closure rate with the traffic.
The accuracy requirements are based on the basic surveillance needs. Originally, they were going to require a higher accuracy and integrity because they would eventually be needed in certain applications. The FAA was talked out of these stringent requirements in the final rule, although if an aircraft is to participate in some of the applications, it will need to meet the accuracy requirements to play in that ballgame. The basic requirements are in the rule 91.227 and specify:
(c) ADS-B Out Performance Requirements for NACP, NACV, NIC, SDA, and SIL--
(1) For aircraft broadcasting ADS-B Out as required under Sec. 91.225 (a) and (b)--
(i) The aircraft's NACP must be less than 0.05 nautical miles;
(ii) The aircraft's NACV must be less than 10 meters per second;
(iii) The aircraft's NIC must be less than 0.2 nautical miles;
(iv) The aircraft's SDA must be 2; and
(v) The aircraft's SIL must be 3.
(2) Changes in NACP, NACV, SDA, and SIL must be broadcast within 10 seconds.
(3) Changes in NIC must be broadcast within 12 seconds.
NACp is position accuracy, NACv is velocity accuracy, NIC is navigational integrity limits. All these are dynamic parameters and continually broadcast by the aircraft.
SIL describes the Position Source and a value of 3 means that the position source is certified to have a probability of exceeding the NIC containment radius by no more than 1 in 10,000,000 on a flight hour or per sample basis. Normally this is a static value. A portable ADS-B Out system is not certified and is supposed to be 0 and ignored by a certified receiver.
The SDA describes the ADS-B Out unit and must not have an undetected fault causing false or misleading information at a rate any greater than 1 x 10^-7 per flight hour. Only certified equipment may satisfy this criteria. It is a characteristic of the equipment and is static.
If the ADS-B Out system is compliant with either RTCA DO260B (1090ES) or DO282B (UAT) but one of the parameters above specified above are not within tolerances allowed, ATC will not use the position for any surveillance.