Severity: Warning
Message: fopen(/home/answnniz/solutionspile.com/system/sessions/ci_session901b8b16aa880dccb87431894347d321ae49c5bc): failed to open stream: Disk quota exceeded
Filename: drivers/Session_files_driver.php
Line Number: 176
Backtrace:
File: /home/answnniz/solutionspile.com/index.php
Line: 367
Function: require_once
Severity: Warning
Message: session_start(): Failed to read session data: user (path: /home/answnniz/solutionspile.com/system/sessions)
Filename: Session/Session.php
Line Number: 143
Backtrace:
File: /home/answnniz/solutionspile.com/index.php
Line: 367
Function: require_once
function [t,v,m] = rocket_euler(delt,simend,params) %%This function simulates a rocket's velocity during launch using Euler's %method. %%Inputs: delt - step size for Euler's method (s) % simend - final simulation time (s) % params - launch parameters (structure variable, with fields c, m0, and mdot) %%Outputs: t - time vector for simulation (s) % v - velocity vector of simulation (m/s) % m - mass vector of simulation (kg) %%Author: Mx. Gator %Get the variables we need out of the params structure variable provided by the user c = params.c; %thrust coefficient (m/s) m0 = params.m0; %initial mass (kg) mdot = params.mdot; %fuel burn rate (kg/s) end