Integrated navigation system for the second sharp edge flight experiment (SHEFEX-2)

Advances in the Astronautical Sciences

Volumn 131, Issue , 2008, Pages 721-731

  Theil, Stephan ^b   Schlotterer, Markus ^b   Conradt, Michael ^b   Hallmann, Marcus ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b NONE

Author keywords

[No Author keywords available]

Indexed keywords

ANDOYA ROCKET RANGES; ATTITUDE MEASUREMENTS; FACETED SURFACES; FLIGHT PATHS; GPS RECEIVERS; HYPERSONIC FLIGHTS; INERTIAL MEASUREMENT UNITS; INTEGRATED NAVIGATION SYSTEMS; INTEGRATED NAVIGATIONS; LAUNCH VIBRATIONS; NAVIGATION SOLUTIONS; PROTECTION SYSTEMS; RE-ENTRY MISSIONS; RE-ENTRY VEHICLES; SHARP EDGE FLIGHT EXPERIMENTS; SHARP EDGES; SIDE-SLIP ANGLES; STAR TRACKERS;

AIRCRAFT INSTRUMENTS; EXPERIMENTS; FLIGHT DYNAMICS; GLOBAL POSITIONING SYSTEM; INERTIAL NAVIGATION SYSTEMS; LANDFORMS; LAUNCHING; REENTRY; UNITS OF MEASUREMENT;

NAVIGATION;

EID: 62949215616     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Markus Schlotterer. Navigation System for Reusable Launch Vehicle. In 31th Annual AAS Guidance and Control Conference, Breckenridge, Colorado, February 2008.
2. Markus Schlotterer. Robuste Schatzung und Sensorfusion zur Navigation von wiederverwendbaren Raumtransportern. PhD thesis, Universität Bremen, Fachbereich Produktionstechnik, 2008.
3. H. Weihs, J. Longo, and A. Gülhan. The sharp edge flight experiment shefex. In 4th European Workshop on Hot Structures and TPS for Space Vehicles, Palermo, Italy, November 2002.
4. Hendrik Weihs, John Turner, and Hörschgen Marcus. SHEFEX II -The Next Step within Flight Testing of Re-entry Technology. In 57th International Astronautical Congress of the International Astronautical Federation. IAF, October 2006.