HASI ACC XSERVO higher level product derivation ------------------------------------------------ Vertical profiles of atmospheric *density*, *pressure* and *temperature* have been derived during entry using accelerometric data considering the drag force exerted by the atmosphere on the Probe and using the assumption of hydrostatic equilibrium and the perfect gas law (refer to ZARNECKIETAL2001 [RD1] and FULCHIGNONIETAL2002). The probe *trajectory* and *attitude* can be reconstructed by analysing vehicle acceleration. The profile of axial and normal accelerations during the Huygens entry and descent in Titan's atmosphere will be used in order to retrieve the probe entry track, velocity and altitude profiles, and attitude, during the high-speed entry phase (ref. FULCHIGNONIETAL2002). The *Huygens auxiliary data* (e.g.reference dimentions, mass, CoG, products of Inertia evolution, parachute characteristics and the Huygens aerodynamical database) necessary to for post flight analysis have been provided by the Project and are archived in the Huygens HK data set. ------------ ENTRY ------------ Starting from the *acceleration* profile of the Huygens probe, *Vertical velocity* and *altitude* profile has been derived from trajectory reconstruction by double integration. Vertical profiles of atmospheric *density*, pressure and temperature have been derived during entry using accelerometric data considering the drag force exerted by the atmosphere on the Probe and using the assumption of hydrostatic equilibrium and the perfect gas law (refer to ZARNECKIETAL2001 [RD1] and FULCHIGNONIETAL2002). -------------- DESCENT -------------- Altitude and vertical Velocity profiles as derived from trajectory reconstruction during descent Altitude and vertical Velocity profiles have been derived by Kalman filtering relying mainly on reverse HASI Servo Accelerometer integration from impact up to start of the descent phase. In order to contain altitude uncertainties related to direct double integration, probe dynamics has been modeled by propagating probe motion through state equations, and is corrected with both accelerometer data and PPI total pressure measurements (which contain the possible drift in descent velocity) [Bettanini]