9 dof parafoil/payload simulator development and validation

AIAA Modeling and Simulation Technologies Conference and Exhibit

Volumn , Issue , 2003, Pages

  Mooij, E ^a   Wijnands, Q G J ^a,b   Schat, B ^a  

^a AIRBUS DEFENCE AND SPACE   (Germany)

^b EUROPEAN SPACE AGENCY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

DEGREES OF FREEDOM (MECHANICS); EQUATIONS OF MOTION; FLIGHT DYNAMICS; FREE FLIGHT; SHOVELS;

DEGREE OF FREEDOM; FLIGHT DYNAMICS MODEL; FLIGHT ENVIRONMENT; OPEN-LOOP SIMULATIONS; SIX DEGREES OF FREEDOM; SMALL PARAFOIL AUTONOMOUS DELIVERY SYSTEMS; STANDARD ATMOSPHERES; SUSPENSION LINES;

SIMULATORS;

EID: 85087600615     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-5459     Document Type: Conference Paper

References (5)

1. Baumgarte, J., "Stabilization of constraints and integrals of motion", Computer Methods in Applied Mechanics and Engineering, Vol. 1, pp-1-16, 1972.
2. Haug, E.J., Computer aided kinematics and dynamics of mechanical systems, Volume 1: Basic methods, Allyn and Bacon, Needham Heights, Massachusetts, 1989.
3. Mooij, E., Aerospace-plane flight dynamics: analysis of guidance and control concepts, PhD thesis, Delft University of Technology, Faculty of Aerospace Engineering, 1998.
4. Mooij, E. and Wijnands, Q.G.J., "Generic Attitude and Orbit Control Simulator development supporting the AOCS software life cycle", From: 7th International Workshop on Simulation for European Space Programmes, November 12-14, 2002, Noordwijk, The Netherlands.
5. Wegereef, J.W. and Jentink, H. SPADES: a parafoil delivery system for payloads up to 200 kg, AIAA-2003-2110, from: 17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, Monterey, CA, 19-22 May 2003.