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ESTEC - Oct 3rd 2006 ASTRIUM ASTRIUM Space Transportation Astrodynamics tools overview T. JEAN-MARIUS [email protected]

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Page 1: ASTRIUM Space Transportation - European Space Agencytrajectory.estec.esa.int/Astro/3rd-astro-workshop...ESTEC - Oct 3rd 2006 ASTRIUM ASTRIUM Space Transportation Astrodynamics tools

ESTEC - Oct 3rd 2006

ASTRIUM

ASTRIUM Space Transportation

Astrodynamics tools overview

T. JEAN-MARIUS

[email protected]

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ASTRIUM

TD

BL Defence

B. Duthoit

TL

BL Launchers

M. Freuchet

TO

BL Orbital &

Reusable

Systems

M. Menking

TP

BL Propulsion &

Equipment

A. Rohne

TE

Competence

Centre

P. Verzat

TB

FU Business

Development

S.F. Graul

Staff

P. Puy-Montbrun

President E. DUDOK

CEO A. CHARMEAU

SPACE TRANSPORTATION

Associated Managt Committee Members

L. Martinez* Finance & ControlM. Sesques* Human ResourcesM. Spude* Communication

Chief Technical Officer

G. Bréard

ASTRIUM

Space Transportation Satellites Services

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ASTRIUMCompetence CentreOrganisation Chart

TECompetence Centre

P. VERZAT

TE41ATV Functional

Engineering & Software

F. Dubuc

TE42Data Management

& Software

P. Cormery

TE43Mission Analysis

Navigation Systems

Th. Jean-Marius

TE44Guidance &

Control Systems

P. Caye

TE53

Avionics Engineering

J. Schneegans

TE54GNC & On board S/W Engineering

U. Westerholt

TE3Thermal Mechanical

Engineering

TE4

GNC & Functional Engineering

Ch. Vallet

TE5

Engineering Centre

J. Bott

TE6

Elec. Engineering, Ground Facilities,

Qualification

TE7Integration & Production

>150 pers

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ASTRIUMASTRIUM-ST is a prime contractor

Mission Analysis is a key competence in its

System Engineering activities

SPECTRUM OF RELATED ACTIVITIES

� System & vehicle architecture conceptual design

� Scenario definitions & Operations

� Reference trajectory computation

� Sizing trajectory computation

� Main sub-system requirement allocations

� Scenario validation through simulations & sensitivity analysis

� Mission preparation & associated S/Ws

PRIMESHIP on vehicles: A5, ATV, Ballistic Missileson demonstrators: Phoenix, ARD

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ASTRIUMWhere Mission Analysis Teams act

Concept

definition

Preliminary

design high level

recommandations

Sub-systems

specification

contribution

Flight strategy

design

Flight strategy

tuning

Mission

Preparation

Concept/Design, Scenarios, Sizing trajectories, Performance & Budget

assessment

Configuration DOF

PHASE 0 PHASE A PHASE A/B PHASE B/C/D PHASE C/D ALL PHASES

system loops

Guidance feasibility, design and performance assessment Phases

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ASTRIUM

Mission Analysis

Transient flight

phases

Thermal

studies

Structural &

Mechanical

studies

« Stage »

design

Aerodynamics

Propulsion

SIZING

Guidance

Navigation

Control

FLIGHT CONTROL

Avionics

Ref. trajectory

Specifications

Constraints

Data

Software

customisation

Mission Analysis

Page 7: ASTRIUM Space Transportation - European Space Agencytrajectory.estec.esa.int/Astro/3rd-astro-workshop...ESTEC - Oct 3rd 2006 ASTRIUM ASTRIUM Space Transportation Astrodynamics tools

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ASTRIUMMission Analysis

at ASTRIUM Transportation

BALLISTIC MISSILES(M51 & NG Ballistic

Missiles, Threats)• Submarine path• Atmospheric path• Sub-orbital fly

• Objects re-entry

REUSABLELAUNCHERS(Everest, Hoper,

FLPP, Ares)• Ascent phases• Orbital phases• Re-entry• Landing

LAUNCHERS (A5, Vega, NGL, PAV,

competitors)• Lift off phase• Atmospheric path

• Orbital phase• Payload delivery

GUIDED RE-ENTRY & LANDING VEHICLES(Lifting body, ARD,

Lander, Phoenix, Probes,Military Weapons)

• De-orbitation

• Hypersonic reentry• Supersonic entry• Parafoil/chute phase• Powered/flying landing

MISSILE DEFENSE, KILL VEHICLES• Launch• Target designation,

recognition & selection• Terminal Guidance• Interception

ORBITAL SPACECRAFT

(ATV, CARV, CEV, On Orbit Servicing)• Injection• Orbital phase

• Phasing, Closing• Autonomous RdV or Proximity Ops• De-orbitation

ESA / CNES / DLR / MODs / NATO

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ASTRIUMTools presentations

ASTRIUM Transportation

BALLISTIC MISSILES

REUSABLE

LAUNCHERS

LAUNCHERS

GUIDED RE-ENTRY & LANDING VEHICLES

MISSILE DEFENSE, KILL VEHICLES

ORBITAL SPACECRAFT

ATPE

ITI

GOAL

PAV FES

SITHAR

Simu Lander

OPTIRV/GORBI

TOPE

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ASTRIUMCONCLUSION

As a PRIME for space transportation & along years,ASTRIUM-ST has developed its own astrodynamics tools for its customers and their project needs.

Those cover a wide space transportation spectrum,

The tools for operationnal or in-development vehicleshave been approved by customer experts to be certifiedas reference tools(e.g. ONERA, LRBA, CNES benchmarks…)

The major ones are flight qualified.

Flexibility and autonomy on mission analysis toolsis key for ASTRIUM-ST.

Continuous efforts are thus made to sustain customer project needs & our own R&Ds for independant mission analysis purposes, basedon home or commercial core optimizers.

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ASTRIUMASTRIUM Space Transportation presentations

Presentations Date Hour Author Room

Generic all purpose ASTRIUM ST reference trajectory

optimisation tools

Oct 3rd 14h00 N. Delattre Newton

Aeroassit, entry & descent ATPE tool for Planetary Exploration for

Venus, Europa, Earth and Exomars Mission)

Oct 3rd 14h30 E. Ferreira Newton

Interplanetary Path Early Design tools at ASTRIUM ST Oct 4th 12h00 N. Delattre Newton 1

GOAL (Multidisciplinary design tool for expandable launcher) Oct 4th 14h30 N. Delattre Newton 1

Guided Hypersonic Reentry and TAEM Analysis Tools Oct 4th 09h00 E. Ferreira Einstein

SIMU-LANDER : Hazard avoidance & GNC (vision, radar or Lidar)

simulation tool for interplanetary descent and landing

Oct 4th 16h00 T. Jean-Marius Einstein

Minimum-time problem resolution under constraints for low-thrust

stage trajectory computation

Oct 5th 10h00 N. Delattre Newton 1

Toolbox for optimisation of phasing manoeuvres, far and close

rendez-vous flight

Oct 5th 12h00 N. Delattre Einstein

Planetary Ascent Vehicle Functional Engineering Simulator Tool Oct 5th 12h30 T. Jean-Marius Newton 1