'Bob', you're talking here about a Russian-built Tupelov 154, design originally circa late 1960s. The Polish Air Force VIP jet that crashed was the Tu-154M 'Lux' version, built sometime in the 1980s.
Unlikely it would have the sort of sophisticated avionics that include an AutoLand technology. It DID have what we call 'enhanced GPWS', also called 'TAWS'...this is a GPS-linked system that has a database of terrain heights, and man-made obstructions world wide. So, fairly updated. HOWEVER, in the vicinity of the airport, and when the airplane is in the landing configuration, the warnings might not activate, unless way off course, and headed for hills of known obstructions. Trees are NOT programmed in, as it assumes, with gear and flaps extended, that pilot intends to land, and that pilot is avoiding trees.
Further, AutoLand is not available at all airports, and on all runways. It is a very, very specific procedure, and requires more precise ground-based equipment, as well as the onboard equipment.
Onboard requirement for full AutoLand include, among other things, a tripple-redundant AutoPilot system. (Terms 'fail/passive' and 'fail/active' also are important, and define certain visibility minima, and operating parameters).
There is ALWAYS a minimum visibility requirement for AutoLandings, and that is covered in special procedures and training for flight crews who become certified to conduct them.
Tu-154M
The Tu-154M and Tu-154M Lux are the most highly upgraded version, which first flew in 1982 and entered mass production in 1984. It uses more fuel-efficient Soloviev D-30KU-154 turbofans. Together with significant aerodynamic refinement, this led to much lower fuel consumption and therefore longer range, as well as lower operating costs. The aircraft has new double-slotted (instead of triple-slotted) flaps, with an extra 36-degree position (in addition to existing 15, 28 and 45-degree positions on older versions), which allows reduction of noise on approach. It also has a relocated auxiliary power unit and numerous other improvements. Manufacture continued through 2006, and there is still limited manufacturing as of January 2009.(photo link) Max. take-off weight increased first to 100,000 kg (220,462 lb), then to 102,000 kg (224,872 lb). Some aircraft are certified to 104,000 kg (229,281 lb). Tail numbers are 85616 (prototype), production aircraft from 85606 and on (except 85804, which is re-imported Tu-154B-2). About 320 were manufactured. Mass production ended in 2006. No new airframes have been built since the early 1990s, and production since then has involved assembling airplanes from components on hand. This is the most widely used version in the former Soviet states.
en.wikipedia.org...





